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 53465U 26145.58114536 +.00000000 +00000-0 -10376-3 0 00008
2 53465 97.4446 266.6251 0002005 113.5749 246.5689 15.05659444 07
| Epoch (UTC): | 25 May 2026 13:56:50 |
| Eccentricity: | 0.0002005 |
| inclination: | 97.4446° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.6251° |
| argument of perigee: | 113.5749° |
| revolutions per day: | 15.05659444 |
| mean anomaly at epoch: | 246.5689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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