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 52792U 26145.58242653 +.00000000 +00000-0 +23546-3 0 00004
2 52792 49.9946 305.9402 0020187 203.0956 156.9075 14.81288183 01
| Epoch (UTC): | 25 May 2026 13:58:41 |
| Eccentricity: | 0.0020187 |
| inclination: | 49.9946° |
| perigee height: | 611 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 305.9402° |
| argument of perigee: | 203.0956° |
| revolutions per day: | 14.81288183 |
| mean anomaly at epoch: | 156.9075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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