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 53006U 26145.30707200 +.00000000 +00000-0 +11918-4 0 00008
2 53006 53.2144 110.1707 0001193 59.6794 300.4316 15.08837047 06
| Epoch (UTC): | 25 May 2026 07:22:11 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.1707° |
| argument of perigee: | 59.6794° |
| revolutions per day: | 15.08837047 |
| mean anomaly at epoch: | 300.4316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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