RU | EN | ZH --:-- UTC Sign in
Back

VIGORIDE 7

In orbit NORAD 68473 VTRE-1340-2626-3018-1989

Observations 17
Go to map
Back

2026

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

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

17

Observations all time

Mission information
Spacecraft name
VIGORIDE 7
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
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
482.92 km
Apogee
498.62 km
Inclination
97.5°
Period
94.5 min
Semi-major axis
6868.9 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68473U 26067BK  26287.15924492  .00009170  00000-0  38082-3 0  9991
2 68473  97.4694 245.0642 0011427  91.1401 269.1145 15.23995096 30047
Copy content
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 09:06:47 VIGORIDE-7
NORAD 68473 		HULIANWANG JISHU SHIYAN 10D
NORAD 69323 		4.154 6.58 2.3e-07
2026-10-15 13:34:22 YAOGAN-35 05A
NORAD 53760 		VIGORIDE-7
NORAD 68473 		4.596 9.54 1.7e-07
2026-10-15 20:55:21 OBJECT A
NORAD 65259 		VIGORIDE-7
NORAD 68473 		0.779 15.07 2.6e-06
2026-10-16 11:18:58 QMR-KWT-2 (RS95S)
NORAD 67291 		VIGORIDE-7
NORAD 68473 		3.743 12.84 1.9e-07
2026-10-16 11:32:22 VIGORIDE-7
NORAD 68473 		SIMSAT 1
NORAD 26365 		4.971 15.23 6.0e-08
2026-10-16 18:28:40 VIGORIDE-7
NORAD 68473 		RAVEN
NORAD 69016 		1.702 7.77 1.3e-06
2026-10-17 10:04:25 GHGSAT-C13
NORAD 64548 		VIGORIDE-7
NORAD 68473 		1.810 14.76 5.4e-07
2026-10-18 12:04:12 SATMAR
NORAD 64551 		VIGORIDE-7
NORAD 68473 		4.550 14.83 8.5e-08
2026-10-18 22:24:33 IRIDE-MS1-EAGLET 2-5
NORAD 66699 		VIGORIDE-7
NORAD 68473 		2.582 12.62 4.1e-07
2026-10-19 01:00:50 STARLINK-5534
NORAD 56477 		VIGORIDE-7
NORAD 68473 		0.542 5.19 4.3e-04
2026-10-19 03:08:10 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		VIGORIDE-7
NORAD 68473 		2.286 12.62 5.2e-07
2026-10-20 08:16:59 TYCHE
NORAD 60496 		VIGORIDE-7
NORAD 68473 		1.904 12.97 7.3e-07
2026-10-20 21:31:28 ZHANGHENG 1-02 (CSES-2)
NORAD 64393 		VIGORIDE-7
NORAD 68473 		2.253 14.97 3.2e-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