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 53142U 26145.55826171 +.00000000 +00000-0 +12525-4 0 00000
2 53142 53.2117 189.0180 0001246 65.2444 294.8678 15.08839214 06
| Epoch (UTC): | 25 May 2026 13:23:53 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.0180° |
| argument of perigee: | 65.2444° |
| revolutions per day: | 15.08839214 |
| mean anomaly at epoch: | 294.8678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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