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TEVEL2-5

In orbit NORAD 63214 VYVA-6255-9438-9598-3516

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

69

Observations all time

Mission information
Spacecraft name
TEVEL2-5
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-03-15 06:43:00
Separation time
Last observers
Observer
Time of receipt
2026-02-02 20:56:23 UTC
2026-02-01 19:43:33 UTC
2026-01-31 20:09:34 UTC
2025-08-18 08:05:54 UTC
2025-08-16 07:11:49 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
445.51 km
Apogee
451.79 km
Inclination
97.4°
Period
93.6 min
Semi-major axis
6826.8 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 63214U 25052E   26282.96861882  .00021096  00000-0  56359-3 0  9997
2 63214 97.3740 179.6655 0004596 73.3664 286.8086 15.38105702 87735
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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
2026-10-11 06:48:01 TEVEL2-5
NORAD 63214
ELECTRON KICK STAGE R/B
NORAD 54228
3.700 13.53 1.8e-07
2026-10-11 08:58:18 STARLINK-3391
NORAD 51117
TEVEL2-5
NORAD 63214
3.853 14.40 4.1e-06
2026-10-11 11:04:04 TSAT-1A
NORAD 59442
TEVEL2-5
NORAD 63214
4.101 7.20 2.4e-07
2026-10-11 14:25:16 GAOFEN-9 04
NORAD 46025
TEVEL2-5
NORAD 63214
1.210 15.11 1.1e-06
2026-10-12 00:41:44 TEVEL2-5
NORAD 63214
SL-3 R/B
NORAD 12586
3.406 14.70 4.4e-07
2026-10-12 17:46:47 STARLINK-4764
NORAD 53827
TEVEL2-5
NORAD 63214
3.791 14.22 4.4e-06
2026-10-13 09:26:42 STARLINK-5177
NORAD 54090
TEVEL2-5
NORAD 63214
4.631 12.65 3.9e-06
2026-10-13 14:57:18 TEVEL2-5
NORAD 63214
CZ-4C R/B
NORAD 59729
3.975 14.67 1.2e-07
2026-10-13 20:22:20 STARLINK-5184
NORAD 54087
TEVEL2-5
NORAD 63214
4.934 12.80 3.4e-06
2026-10-14 04:03:47 STARLINK-3872
NORAD 52453
TEVEL2-5
NORAD 63214
4.664 6.46 5.6e-06
2026-10-14 11:38:52 AETHER-2
NORAD 58299
TEVEL2-5
NORAD 63214
3.916 15.13 1.0e-07
2026-10-15 09:11:05 TEVEL2-5
NORAD 63214
CZ-4C R/B
NORAD 52913
3.592 11.21 2.5e-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