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 62585U 26145.59529325 +.00000000 +00000-0 +98155-4 0 00009
2 62585 54.9895 10.2792 0013660 50.3129 309.9030 13.80608498 06
| Epoch (UTC): | 25 May 2026 14:17:13 |
| Eccentricity: | 0.0013660 |
| inclination: | 54.9895° |
| perigee height: | 952 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 10.2792° |
| argument of perigee: | 50.3129° |
| revolutions per day: | 13.80608498 |
| mean anomaly at epoch: | 309.9030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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