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 64950U 26145.38059199 +.00000000 +00000-0 -14805-4 0 00002
2 64950 97.4510 9.2645 0001964 74.2960 285.8484 15.05647706 06
| Epoch (UTC): | 25 May 2026 09:08:03 |
| Eccentricity: | 0.0001964 |
| inclination: | 97.4510° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.2645° |
| argument of perigee: | 74.2960° |
| revolutions per day: | 15.05647706 |
| mean anomaly at epoch: | 285.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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