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Spacevan-002

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

Observations 0
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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
501.92 km
Apogee
505.34 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6881.8 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:42 UTC
Two-line elements (TLE)
1 68424U 26067J   26281.84595773  .00004827  00000-0  22909-3 0  9998
2 68424  97.4656 238.8036 0002482  45.1661 314.9775 15.19728127 29192
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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
2026-10-12 01:18:40 SPACEVAN-002
NORAD 68424 		RASSVET-3 25
NORAD 100091 		2.929 11.94 3.5e-07
2026-10-12 07:37:56 SPACEVAN-002
NORAD 68424 		RASSVET-3 27
NORAD 100093 		4.029 11.98 1.8e-07
2026-10-12 17:55:30 SPACEVAN-002
NORAD 68424 		SHARJAH-SAT-2
NORAD 68444 		4.196 0.04 2.5e-07
2026-10-12 18:42:45 SPACEVAN-002
NORAD 68424 		SHARJAH-SAT-2
NORAD 68444 		4.552 0.04 2.1e-07
2026-10-12 21:04:19 SPACEVAN-002
NORAD 68424 		OUT OF THE BOX (OOTB)
NORAD 68428 		3.266 0.02 4.1e-07
2026-10-12 22:07:49 SPACEVAN-002
NORAD 68424 		COSMOS 374 DEB
NORAD 4699 		1.183 14.94 1.2e-06
2026-10-13 04:27:29 STARLINK-5072
NORAD 55758 		SPACEVAN-002
NORAD 68424 		1.659 15.08 1.7e-05
2026-10-13 06:31:30 ZIYUAN 3-03 (ZY 3-03)
NORAD 45939 		SPACEVAN-002
NORAD 68424 		1.912 12.37 7.8e-07
2026-10-14 02:12:39 SPACEVAN-002
NORAD 68424 		CP5
NORAD 38763 		4.489 13.45 1.2e-07
2026-10-14 10:27:59 YAOGAN-39 04B
NORAD 58143 		SPACEVAN-002
NORAD 68424 		4.315 11.88 1.6e-07
2026-10-15 20:56:55 ZORKIY-2M 1
NORAD 57177 		SPACEVAN-002
NORAD 68424 		4.169 11.68 1.7e-07
2026-10-16 04:50:21 LYRA-1
NORAD 62664 		SPACEVAN-002
NORAD 68424 		2.662 12.72 3.8e-07
2026-10-16 23:00:40 FLOCK 4H-3
NORAD 66706 		SPACEVAN-002
NORAD 68424 		1.948 12.72 7.2e-07
2026-10-17 07:02:39 STARLINK-5507
NORAD 55638 		SPACEVAN-002
NORAD 68424 		4.520 13.03 3.9e-06
2026-10-17 10:51:39 ALSAT-3B
NORAD 67646 		SPACEVAN-002
NORAD 68424 		3.879 12.77 1.8e-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