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 62254U 26145.46275117 +.00000000 +00000-0 +13318-3 0 00002
2 62254 89.0103 24.7660 0016252 80.4082 279.8904 13.51009553 06
| Epoch (UTC): | 25 May 2026 11:06:21 |
| Eccentricity: | 0.0016252 |
| inclination: | 89.0103° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.7660° |
| argument of perigee: | 80.4082° |
| revolutions per day: | 13.51009553 |
| mean anomaly at epoch: | 279.8904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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