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 65290U 26145.59575638 +.00000000 +00000-0 +53149-2 0 00005
2 65290 97.4498 198.1023 0002121 94.7596 265.3874 15.05802519 06
| Epoch (UTC): | 25 May 2026 14:17:53 |
| Eccentricity: | 0.0002121 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1023° |
| argument of perigee: | 94.7596° |
| revolutions per day: | 15.05802519 |
| mean anomaly at epoch: | 265.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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