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 65810U 26145.58969841 +.00000000 +00000-0 +11241-2 0 00002
2 65810 97.4518 8.4063 0003409 85.4356 274.7261 15.05691568 09
| Epoch (UTC): | 25 May 2026 14:09:09 |
| Eccentricity: | 0.0003409 |
| inclination: | 97.4518° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 8.4063° |
| argument of perigee: | 85.4356° |
| revolutions per day: | 15.05691568 |
| mean anomaly at epoch: | 274.7261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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