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 53001U 26145.17826707 +.00000000 +00000-0 +54699-4 0 00005
2 53001 53.2122 110.7485 0001502 80.7492 279.3670 15.08841441 00
| Epoch (UTC): | 25 May 2026 04:16:42 |
| Eccentricity: | 0.0001502 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.7485° |
| argument of perigee: | 80.7492° |
| revolutions per day: | 15.08841441 |
| mean anomaly at epoch: | 279.3670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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