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 62366U 26145.58572781 +.00000000 +00000-0 +12912-3 0 00005
2 62366 44.9809 62.2954 0005487 285.0308 74.9917 13.99179109 03
| Epoch (UTC): | 25 May 2026 14:03:26 |
| Eccentricity: | 0.0005487 |
| inclination: | 44.9809° |
| perigee height: | 893 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 62.2954° |
| argument of perigee: | 285.0308° |
| revolutions per day: | 13.99179109 |
| mean anomaly at epoch: | 74.9917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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