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 52268U 26145.31856201 +.00000000 +00000-0 +63389-4 0 00003
2 52268 53.2147 125.0424 0001311 80.7027 279.4113 15.08836415 03
| Epoch (UTC): | 25 May 2026 07:38:43 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.0424° |
| argument of perigee: | 80.7027° |
| revolutions per day: | 15.08836415 |
| mean anomaly at epoch: | 279.4113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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