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 62416U 26145.48652679 +.00000000 +00000-0 +19103-2 0 00003
2 62416 43.0012 64.3124 0001330 52.6271 307.4717 15.70899482 03
| Epoch (UTC): | 25 May 2026 11:40:35 |
| Eccentricity: | 0.0001330 |
| inclination: | 43.0012° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 64.3124° |
| argument of perigee: | 52.6271° |
| revolutions per day: | 15.70899482 |
| mean anomaly at epoch: | 307.4717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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