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 62895U 26145.56093876 +.00000000 +00000-0 +85380-3 0 00002
2 62895 43.0006 251.1265 0001266 268.0575 92.0132 15.27599560 01
| Epoch (UTC): | 25 May 2026 13:27:45 |
| Eccentricity: | 0.0001266 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.1265° |
| argument of perigee: | 268.0575° |
| revolutions per day: | 15.27599560 |
| mean anomaly at epoch: | 92.0132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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