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 65387U 26145.40198380 +.00000000 +00000-0 +50161-3 0 00009
2 65387 97.4494 16.7766 0002176 100.2593 259.8879 15.05653500 05
| Epoch (UTC): | 25 May 2026 09:38:51 |
| Eccentricity: | 0.0002176 |
| inclination: | 97.4494° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.7766° |
| argument of perigee: | 100.2593° |
| revolutions per day: | 15.05653500 |
| mean anomaly at epoch: | 259.8879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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