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 52700U 26145.45836287 +.00000000 +00000-0 +16704-4 0 00000
2 52700 53.2142 164.1310 0001148 81.2341 278.8781 15.08843321 08
| Epoch (UTC): | 25 May 2026 11:00:02 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.1310° |
| argument of perigee: | 81.2341° |
| revolutions per day: | 15.08843321 |
| mean anomaly at epoch: | 278.8781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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