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 61053U 26145.42829583 +.00000000 +00000-0 +11088-4 0 00009
2 61053 53.1580 292.8207 0001015 87.2738 272.8396 15.69709028 05
| Epoch (UTC): | 25 May 2026 10:16:44 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.1580° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 292.8207° |
| argument of perigee: | 87.2738° |
| revolutions per day: | 15.69709028 |
| mean anomaly at epoch: | 272.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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