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 62479U 26145.47343235 +.00000000 +00000-0 +76641-3 0 00007
2 62479 43.0022 295.1590 0001677 263.6033 96.4628 15.27594240 00
| Epoch (UTC): | 25 May 2026 11:21:44 |
| Eccentricity: | 0.0001677 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.1590° |
| argument of perigee: | 263.6033° |
| revolutions per day: | 15.27594240 |
| mean anomaly at epoch: | 96.4628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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