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 61635U 26145.54247297 +.00000000 +00000-0 +22999-4 0 00007
2 61635 43.0034 80.1667 0001213 261.5878 98.4837 15.27575740 01
| Epoch (UTC): | 25 May 2026 13:01:09 |
| Eccentricity: | 0.0001213 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.1667° |
| argument of perigee: | 261.5878° |
| revolutions per day: | 15.27575740 |
| mean anomaly at epoch: | 98.4837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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