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HADES-SA

In orbit NORAD 68446 MIAF-5680-8845-1005-1215 Spain

Observations 237
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Time in UTC

08:34

Next pass · Индия · 8°

15.10 11:51

Scheduled · Сампо-435 [R1NAV]

11

Observations over 30 days

85%

Successful observations

44k

Frames, latest 2026-10-11 13:21 UTC

Mission information
Spacecraft name
HADES-SA
Other names
SpinnyONE
Website
https://www.amsat-ea.org/
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
2026-03-29 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
489.06 km
Apogee
499.62 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6872.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68446U 26067AG  26287.10716842  .00025311  00000-0  10819-2 0  9996
2 68446  97.4544 244.0231 0007687  39.1381 321.0410 15.22808484 30008
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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
2026-10-15 18:20:16 GAOFEN-14 02
NORAD 66175 		HADES-SA (SPINNYONE)
NORAD 68446 		4.424 12.92 1.4e-07
2026-10-17 12:07:48 TRANSPORTER-15 OBJECT CN
NORAD 66750 		HADES-SA (SPINNYONE)
NORAD 68446 		4.257 12.69 1.5e-07
2026-10-17 14:37:35 STARLINK-5507
NORAD 55638 		HADES-SA (SPINNYONE)
NORAD 68446 		4.680 12.96 3.6e-06
2026-10-18 03:54:55 HADES-SA (SPINNYONE)
NORAD 68446 		CZ-4 DEB
NORAD 35375 		4.830 10.78 1.4e-07
2026-10-18 12:36:46 HADES-SA (SPINNYONE)
NORAD 68446 		SL-3 R/B
NORAD 19046 		4.768 3.42 5.2e-07
2026-10-18 15:33:39 STARLINK-5908
NORAD 55951 		HADES-SA (SPINNYONE)
NORAD 68446 		4.804 15.07 2.1e-06
2026-10-19 00:23:52 TRANSPORTER-15 OBJECT DM
NORAD 66773 		HADES-SA (SPINNYONE)
NORAD 68446 		3.718 12.71 2.0e-07
2026-10-19 23:52:36 HADES-SA (SPINNYONE)
NORAD 68446 		COSMOS 886 DEB
NORAD 18907 		1.880 15.23 4.7e-07
2026-10-20 16:14:52 HADES-SA (SPINNYONE)
NORAD 68446 		GLOBAL-36
NORAD 100682 		2.714 13.99 3.0e-07
2026-10-20 19:45:34 LEMUR-2-LAILA
NORAD 66776 		HADES-SA (SPINNYONE)
NORAD 68446 		3.773 12.76 1.9e-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