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 52357U 26145.58628308 +.00000000 +00000-0 +58914-4 0 00004
2 52357 53.2135 213.9191 0001006 88.6223 271.4884 15.08842843 02
| Epoch (UTC): | 25 May 2026 14:04:14 |
| Eccentricity: | 0.0001006 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 213.9191° |
| argument of perigee: | 88.6223° |
| revolutions per day: | 15.08842843 |
| mean anomaly at epoch: | 271.4884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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