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 52538U 26145.26888351 +.00000000 +00000-0 -11172-3 0 00001
2 52538 53.2135 145.3430 0001048 80.7513 279.3597 15.08849958 00
| Epoch (UTC): | 25 May 2026 06:27:11 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 145.3430° |
| argument of perigee: | 80.7513° |
| revolutions per day: | 15.08849958 |
| mean anomaly at epoch: | 279.3597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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