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 51053U 26145.56335581 +.00000000 +00000-0 +54252-3 0 00002
2 51053 97.2843 225.6138 0001015 68.2098 291.9272 15.68095056 03
| Epoch (UTC): | 25 May 2026 13:31:13 |
| Eccentricity: | 0.0001015 |
| inclination: | 97.2843° |
| perigee height: | 364 km |
| apogee height: | 365 km |
| right ascension of ascending node: | 225.6138° |
| argument of perigee: | 68.2098° |
| revolutions per day: | 15.68095056 |
| mean anomaly at epoch: | 291.9272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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