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 53013U 26145.26750578 +.00000000 +00000-0 +15440-5 0 00002
2 53013 53.2133 100.3486 0001172 90.2467 269.8659 15.08842534 07
| Epoch (UTC): | 25 May 2026 06:25:12 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.3486° |
| argument of perigee: | 90.2467° |
| revolutions per day: | 15.08842534 |
| mean anomaly at epoch: | 269.8659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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