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 52702U 26145.35537148 +.00000000 +00000-0 -68412-4 0 00009
2 52702 53.2123 164.9836 0001144 101.3070 258.8050 15.08851851 03
| Epoch (UTC): | 25 May 2026 08:31:44 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.9836° |
| argument of perigee: | 101.3070° |
| revolutions per day: | 15.08851851 |
| mean anomaly at epoch: | 258.8050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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