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 62335U 26145.64945696 +.00000000 +00000-0 +42105-3 0 00004
2 62335 97.5273 93.4418 0002457 84.8774 275.2737 15.14121872 04
| Epoch (UTC): | 25 May 2026 15:35:13 |
| Eccentricity: | 0.0002457 |
| inclination: | 97.5273° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 93.4418° |
| argument of perigee: | 84.8774° |
| revolutions per day: | 15.14121872 |
| mean anomaly at epoch: | 275.2737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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