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 52836U 26145.66668980 +.00000000 +00000-0 +11229-1 0 00000
2 52836 53.2251 42.8557 0001518 84.4838 24.0954 15.38077342 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001518 |
| inclination: | 53.2251° |
| perigee height: | 451 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 42.8557° |
| argument of perigee: | 84.4838° |
| revolutions per day: | 15.38077342 |
| mean anomaly at epoch: | 24.0954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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