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 52848U 26145.43772895 +.00000000 +00000-0 +53388-3 0 00003
2 52848 53.2114 49.5842 0001355 98.5936 261.5209 15.08790531 05
| Epoch (UTC): | 25 May 2026 10:30:19 |
| Eccentricity: | 0.0001355 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.5842° |
| argument of perigee: | 98.5936° |
| revolutions per day: | 15.08790531 |
| mean anomaly at epoch: | 261.5209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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