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GITAI-SC1

In orbit NORAD 62388 IFBU-4266-8266-9018-9039 United States of America

Observations 0
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2024

Falcon 9 Block 5 | Bandwagon 2 (Dedicated Mid-Inclination Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
GITAI-SC1
Other names
SC1
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 | Bandwagon 2 (Dedicated Mid-Inclination Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2024-12-20 11:34:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.74 km
Apogee
502.07 km
Inclination
45.0°
Period
94.6 min
Semi-major axis
6878.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:44 UTC
Two-line elements (TLE)
1 62388U 24247M   26284.03552290  .00006077  00000-0  27056-3 0  9997
2 62388  45.0034  44.7380 0002418 272.8836  87.1768 15.22341734100383
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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 23:28:41 GITAI-SC1
NORAD 62388 		IRIDE-MS1-EAGLET 2-3
NORAD 66697 		3.369 8.17 3.4e-07
2026-10-13 07:08:57 YAOGAN-36 05A
NORAD 57452 		GITAI-SC1
NORAD 62388 		4.795 1.34 1.9e-07
2026-10-13 16:29:41 KANOPUS-V 5
NORAD 43876 		GITAI-SC1
NORAD 62388 		2.704 14.24 2.9e-07
2026-10-13 22:46:56 GITAI-SC1
NORAD 62388 		SITRO-AIS-57
NORAD 67256 		4.632 7.45 1.8e-07
2026-10-14 02:16:06 STARLINK-5633
NORAD 55410 		GITAI-SC1
NORAD 62388 		4.422 11.96 4.6e-06
2026-10-14 03:03:22 STARLINK-5633
NORAD 55410 		GITAI-SC1
NORAD 62388 		3.877 11.97 6.0e-06
2026-10-16 01:11:59 GITAI-SC1
NORAD 62388 		LIZZIESAT-3 (LS-3)
NORAD 63233 		2.651 14.27 2.9e-07
2026-10-16 10:42:21 GITAI-SC1
NORAD 62388 		BRO-21
NORAD 69007 		3.634 14.38 1.5e-07
2026-10-16 21:44:50 GITAI-SC1
NORAD 62388 		HELIOS
NORAD 69021 		4.059 14.39 1.2e-07
2026-10-17 04:51:37 GITAI-SC1
NORAD 62388 		BUZZER-1
NORAD 62609 		4.756 6.74 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