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 55010U 26145.62352524 +.00000000 +00000-0 +86407-3 0 00009
2 55010 97.3165 212.9054 0005716 175.9034 184.2269 15.57132247 04
| Epoch (UTC): | 25 May 2026 14:57:52 |
| Eccentricity: | 0.0005716 |
| inclination: | 97.3165° |
| perigee height: | 392 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 212.9054° |
| argument of perigee: | 175.9034° |
| revolutions per day: | 15.57132247 |
| mean anomaly at epoch: | 184.2269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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