View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65809U 26145.39862049 +.00000000 +00000-0 +30440-3 0 00004
2 65809 97.4487 8.2027 0002463 94.1481 266.0028 15.05657222 09
| Epoch (UTC): | 25 May 2026 09:34:00 |
| Eccentricity: | 0.0002463 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2027° |
| argument of perigee: | 94.1481° |
| revolutions per day: | 15.05657222 |
| mean anomaly at epoch: | 266.0028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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