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 53075U 26145.43442091 +.00000000 +00000-0 -30080-4 0 00004
2 53075 97.4489 325.4366 0001161 106.9591 253.1764 15.05654738 04
| Epoch (UTC): | 25 May 2026 10:25:33 |
| Eccentricity: | 0.0001161 |
| inclination: | 97.4489° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.4366° |
| argument of perigee: | 106.9591° |
| revolutions per day: | 15.05654738 |
| mean anomaly at epoch: | 253.1764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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