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 62253U 26145.63145590 +.00000000 +00000-0 +15691-3 0 00007
2 62253 89.0095 24.6324 0017369 78.9831 281.3273 13.51006885 07
| Epoch (UTC): | 25 May 2026 15:09:17 |
| Eccentricity: | 0.0017369 |
| inclination: | 89.0095° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.6324° |
| argument of perigee: | 78.9831° |
| revolutions per day: | 13.51006885 |
| mean anomaly at epoch: | 281.3273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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