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 61503U 26145.49719830 +.00000000 +00000-0 +00000-0 0 00007
2 61503 0.0453 359.6397 0001128 95.9809 249.2974 1.00267146 07
| Epoch (UTC): | 25 May 2026 11:55:57 |
| Eccentricity: | 0.0001128 |
| inclination: | 0.0453° |
| perigee height: | 35783 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 359.6397° |
| argument of perigee: | 95.9809° |
| revolutions per day: | 1.00267146 |
| mean anomaly at epoch: | 249.2974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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