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 52761U 26145.36688634 +.00000000 +00000-0 +27527-3 0 00002
2 52761 97.6072 292.9094 0017418 192.4170 167.6651 15.44653756 02
| Epoch (UTC): | 25 May 2026 08:48:18 |
| Eccentricity: | 0.0017418 |
| inclination: | 97.6072° |
| perigee height: | 421 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 292.9094° |
| argument of perigee: | 192.4170° |
| revolutions per day: | 15.44653756 |
| mean anomaly at epoch: | 167.6651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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