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 64952U 26145.39720027 +.00000000 +00000-0 +27812-3 0 00000
2 64952 97.4495 9.2382 0001913 91.5082 268.6364 15.05657452 04
| Epoch (UTC): | 25 May 2026 09:31:58 |
| Eccentricity: | 0.0001913 |
| inclination: | 97.4495° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.2382° |
| argument of perigee: | 91.5082° |
| revolutions per day: | 15.05657452 |
| mean anomaly at epoch: | 268.6364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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