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 62316U 26145.55217700 +.00000000 +00000-0 +59857-3 0 00003
2 62316 53.1594 196.7803 0001100 88.2441 271.8687 15.34392057 08
| Epoch (UTC): | 25 May 2026 13:15:08 |
| Eccentricity: | 0.0001100 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 196.7803° |
| argument of perigee: | 88.2441° |
| revolutions per day: | 15.34392057 |
| mean anomaly at epoch: | 271.8687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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