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 62845U 26145.62847242 +.00000000 +00000-0 +58481-3 0 00000
2 62845 42.9999 7.0309 0001369 264.7475 95.3220 15.27591502 00
| Epoch (UTC): | 25 May 2026 15:05:00 |
| Eccentricity: | 0.0001369 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.0309° |
| argument of perigee: | 264.7475° |
| revolutions per day: | 15.27591502 |
| mean anomaly at epoch: | 95.3220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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