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 62083U 26145.68131244 +.00000000 +00000-0 +91927-4 0 00001
2 62083 97.8976 305.2721 0005885 351.7453 8.3657 14.72505527 08
| Epoch (UTC): | 25 May 2026 16:21:05 |
| Eccentricity: | 0.0005885 |
| inclination: | 97.8976° |
| perigee height: | 649 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 305.2721° |
| argument of perigee: | 351.7453° |
| revolutions per day: | 14.72505527 |
| mean anomaly at epoch: | 8.3657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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