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 52369U 26145.41792742 +.00000000 +00000-0 -45452-4 0 00007
2 52369 53.2114 204.6747 0000904 76.2588 283.8504 15.08834734 05
| Epoch (UTC): | 25 May 2026 10:01:48 |
| Eccentricity: | 0.0000904 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.6747° |
| argument of perigee: | 76.2588° |
| revolutions per day: | 15.08834734 |
| mean anomaly at epoch: | 283.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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