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 52122U 26145.16309007 +.00000000 +00000-0 +42068-4 0 00003
2 52122 53.2124 95.8187 0001423 85.2388 274.8766 15.08834856 01
| Epoch (UTC): | 25 May 2026 03:54:50 |
| Eccentricity: | 0.0001423 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.8187° |
| argument of perigee: | 85.2388° |
| revolutions per day: | 15.08834856 |
| mean anomaly at epoch: | 274.8766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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