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GNOMES-5

In orbit NORAD 60574 JOGW-1515-2403-9943-2566

Observations 0
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2024

Falcon 9 Block 5 | Transporter 11 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
GNOMES-5
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 11 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2024-08-16 18:56:00
Separation time
2024-08-16 21:29:41
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
552.36 km
Apogee
564.09 km
Inclination
97.7°
Period
95.9 min
Semi-major axis
6936.4 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 60574U 24149DL  26282.45021226  .00002377  00000-0  18672-3 0  9990
2 60574  97.6995 359.7558 0008457 127.5246 232.6748 15.01838925117308
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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 05:41:35 GNOMES-5
NORAD 60574 		STARLINK-35896
NORAD 66824 		4.102 14.54 3.4e-06
2026-10-11 13:43:04 STARLINK-6059
NORAD 56814 		GNOMES-5
NORAD 60574 		3.050 14.78 5.6e-06
2026-10-13 02:22:55 GNOMES-5
NORAD 60574 		FENGYUN 1C DEB
NORAD 31058 		3.430 8.06 3.2e-07
2026-10-13 15:30:14 GNOMES-5
NORAD 60574 		QPS-SAR-13 (MIKURA-I)
NORAD 100243 		1.445 7.18 1.9e-06
2026-10-13 16:31:58 GNOMES-5
NORAD 60574 		STRIX-7
NORAD 69177 		4.922 10.18 1.4e-07
2026-10-14 05:38:49 STARLINK-6028
NORAD 56818 		GNOMES-5
NORAD 60574 		4.765 14.51 2.5e-06
2026-10-14 12:32:43 GNOMES-5
NORAD 60574 		COSMOS 2292
NORAD 23278 		1.031 15.38 1.4e-06
2026-10-14 14:15:37 GNOMES-5
NORAD 60574 		SL-8 R/B
NORAD 3230 		3.592 14.20 7.9e-07
2026-10-14 18:36:49 GNOMES-5
NORAD 60574 		QPS-SAR-18 (SUSANOO-II)
NORAD 100401 		2.466 13.90 3.6e-07
2026-10-15 18:19:55 GNOMES-5
NORAD 60574 		NOAA 8 DEB
NORAD 38840 		4.172 1.21 2.5e-07
2026-10-16 00:47:28 STARLINK-5859
NORAD 55915 		GNOMES-5
NORAD 60574 		3.096 11.95 9.3e-06
2026-10-16 13:18:50 GRUS-1E
NORAD 47935 		GNOMES-5
NORAD 60574 		1.845 14.84 5.0e-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