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VINDLER 2.2

In orbit NORAD 68484 RKBP-4361-7163-4583-7414

Observations 0
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Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
VINDLER 2.2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.00 km
Apogee
588.58 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6965.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68484U 26067BW  26287.13976759  .00001238  00000-0  12670-3 0  9996
2 68484  97.7678 244.5524 0001132  10.6538 349.4705 14.92298394 29512
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 08:31:31 VINDLER 2.2
NORAD 68484 		ORBCOMM FM111
NORAD 40089 		2.259 10.41 6.6e-07
2026-10-15 12:44:58 VINDLER 2.2
NORAD 68484 		N1-ATLAS
NORAD 68501 		3.180 0.12 4.4e-07
2026-10-15 13:33:13 VINDLER 2.2
NORAD 68484 		N1-ATLAS
NORAD 68501 		2.458 0.12 7.3e-07
2026-10-15 17:34:33 LEMUR-2-SEJONG-3
NORAD 68482 		VINDLER 2.2
NORAD 68484 		4.218 0.08 2.5e-07
2026-10-15 21:57:48 SHIYAN-30 02
NORAD 65852 		VINDLER 2.2
NORAD 68484 		4.485 7.97 1.9e-07
2026-10-15 23:03:38 HUBBLE 7
NORAD 64592 		VINDLER 2.2
NORAD 68484 		2.845 14.67 2.2e-07
2026-10-16 01:33:51 VINDLER 2.2
NORAD 68484 		CZ-6A DEB
NORAD 55902 		2.751 12.48 3.7e-07
2026-10-16 05:51:51 VINDLER 2.2
NORAD 68484 		FENGYUN 1C DEB
NORAD 32137 		2.550 14.88 2.6e-07
2026-10-16 08:26:01 SHIYAN-30 01
NORAD 65851 		VINDLER 2.2
NORAD 68484 		3.140 7.93 3.9e-07
2026-10-16 22:27:19 VINDLER 2.2
NORAD 68484 		CZ-4C DEB
NORAD 37568 		4.557 13.91 1.1e-07
2026-10-17 04:03:19 VINDLER 2.2
NORAD 68484 		CZ-4B DEB
NORAD 26262 		1.001 14.42 1.9e-06
2026-10-17 16:05:59 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		3.794 14.61 1.3e-07
2026-10-17 17:42:33 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		1.909 14.61 5.0e-07
2026-10-17 19:19:07 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		1.157 14.61 1.4e-06
2026-10-17 20:55:40 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		2.733 14.61 2.4e-07
2026-10-17 21:43:57 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		4.083 14.64 1.1e-07
2026-10-17 22:32:14 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		4.693 14.61 8.2e-08
2026-10-17 23:20:31 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		2.082 14.64 4.2e-07
2026-10-18 00:57:05 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		0.664 14.64 4.1e-06
2026-10-18 02:33:38 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		2.233 14.64 3.6e-07
2026-10-18 04:10:12 IRIDE-MS2-HEO-3
NORAD 64568 		VINDLER 2.2
NORAD 68484 		4.237 14.64 1.0e-07
2026-10-19 04:28:12 VINDLER 2.2
NORAD 68484 		IRIDE-MS2-HEO-13
NORAD 68985 		1.766 7.76 1.2e-06
2026-10-19 05:16:29 VINDLER 2.2
NORAD 68484 		IRIDE-MS2-HEO-13
NORAD 68985 		4.805 7.74 1.7e-07
2026-10-19 13:41:03 VINDLER 2.2
NORAD 68484 		CZ-2C DEB
NORAD 28483 		4.180 15.00 9.1e-08
2026-10-19 14:38:31 VINDLER 2.2
NORAD 68484 		ATLAS CENTAUR 2 DEB
NORAD 701 		4.607 11.49 1.5e-07
2026-10-20 11:02:01 E3T-1 (E3TESTER-1)
NORAD 66662 		VINDLER 2.2
NORAD 68484 		2.546 3.81 6.6e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite