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 65630U 26145.44274186 +.00000000 +00000-0 +66103-3 0 00006
2 65630 53.1584 309.7692 0001532 87.1453 272.9725 15.34412489 08
| Epoch (UTC): | 25 May 2026 10:37:32 |
| Eccentricity: | 0.0001532 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.7692° |
| argument of perigee: | 87.1453° |
| revolutions per day: | 15.34412489 |
| mean anomaly at epoch: | 272.9725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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