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

Spacevan-002

In orbit NORAD 68424 ULCN-5659-0953-1472-3090

Observations 0
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

0

Observations all time

Mission information
Spacecraft name
Spacevan-002
Other names
SPACEVAN 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
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
502.18 km
Apogee
505.05 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6881.8 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68424U 26067J   26286.85006361  .00006366  00000-0  30101-3 0  9997
2 68424  97.4673 243.7540 0002084  39.1576 320.9809 15.19732809 29953
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 17:47:32 ZORKIY-2M 1
NORAD 57177 		SPACEVAN-002
NORAD 68424 		0.934 11.68 3.5e-06
2026-10-15 19:21:42 LYRA-1
NORAD 62664 		SPACEVAN-002
NORAD 68424 		3.772 12.72 1.9e-07
2026-10-16 04:05:04 OBJECT A
NORAD 59917 		SPACEVAN-002
NORAD 68424 		4.359 7.37 2.1e-07
2026-10-17 00:35:43 OBJECT AE
NORAD 67276 		SPACEVAN-002
NORAD 68424 		4.656 12.78 1.2e-07
2026-10-18 01:54:25 SPACEVAN-002
NORAD 68424 		RASSVET-3 22
NORAD 100088 		4.750 12.85 1.2e-07
2026-10-18 02:41:50 SPACEVAN-002
NORAD 68424 		RASSVET-3 22
NORAD 100088 		4.776 12.82 1.2e-07
2026-10-18 16:29:05 OBJECT A
NORAD 63291 		SPACEVAN-002
NORAD 68424 		4.129 15.09 9.2e-08
2026-10-18 17:36:16 SPACEVAN-002
NORAD 68424 		COSMOS 2251 DEB
NORAD 40794 		4.314 6.32 2.2e-07
2026-10-19 06:08:22 STARLINK-5925
NORAD 55945 		SPACEVAN-002
NORAD 68424 		4.937 15.08 2.0e-06
2026-10-19 11:03:43 OBJECT AF
NORAD 67277 		SPACEVAN-002
NORAD 68424 		3.953 12.78 1.7e-07
2026-10-20 01:15:37 UMBRA-10
NORAD 60547 		SPACEVAN-002
NORAD 68424 		4.960 13.83 9.3e-08
2026-10-20 15:15:15 STARLINK-5862
NORAD 55920 		SPACEVAN-002
NORAD 68424 		3.152 15.12 4.7e-06

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