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Hubble-5

In orbit NORAD 64840 TGGE-0655-3824-5329-0738 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

274

Observations all time

Mission information
Spacecraft name
Hubble-5
Other names
Scooby
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
2025-06-23 21:25:00
Separation time
2025-06-23 23:43:27
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
578.08 km
Apogee
584.31 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6959.3 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 64840U 25135BT  26284.07055964  .00001943  00000-0  18571-3 0  9998
2 64840 97.7819 37.4794 0004452 324.7980 35.2945 14.94420856 71219
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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 20:19:21 LEMUR-2-HUBBLE-5
NORAD 64840
NOAA 16 DEB
NORAD 41149
4.949 14.96 6.5e-08
2026-10-13 04:41:48 LEMUR-2-HUBBLE-5
NORAD 64840
PSLV R/B
NORAD 43620
4.033 7.28 2.4e-07
2026-10-13 10:29:17 LEMUR-2-HUBBLE-5
NORAD 64840
FLYLAB1
NORAD 68472
1.245 14.69 1.1e-06
2026-10-14 00:57:04 LEMUR-2-HUBBLE-5
NORAD 64840
LEMUR-2-EMARCHIA
NORAD 68492
3.988 14.69 1.1e-07
2026-10-14 05:46:13 LEMUR-2-HUBBLE-5
NORAD 64840
LEMUR-2-PEGGY-2004
NORAD 68479
0.879 14.68 2.3e-06
2026-10-15 01:03:16 LEMUR-2-HUBBLE-5
NORAD 64840
LEMUR-2-POLO-11
NORAD 68493
3.366 14.69 1.6e-07
2026-10-16 04:28:12 LEMUR-2-HUBBLE-5
NORAD 64840
CZ-6A DEB
NORAD 60848
1.886 15.13 4.2e-07
2026-10-16 15:22:04 LEMUR-2-HUBBLE-5
NORAD 64840
LEONAV-1
NORAD 69937
4.237 14.32 1.1e-07
2026-10-17 13:59:11 LEMUR-2-HUBBLE-5
NORAD 64840
CZ-6A DEB
NORAD 55208
4.977 3.26 1.7e-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