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 53823U 26145.07292830 +.00000000 +00000-0 +25625-3 0 00006
2 53823 53.2133 276.2059 0001430 93.1698 266.9458 15.08826268 01
| Epoch (UTC): | 25 May 2026 01:45:01 |
| Eccentricity: | 0.0001430 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 276.2059° |
| argument of perigee: | 93.1698° |
| revolutions per day: | 15.08826268 |
| mean anomaly at epoch: | 266.9458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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