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 23725U 26072.04244076 +.00000000 +00000-0 +50296-3 0 00001
2 23725 25.8134 349.9763 5506252 251.6872 43.2298 4.80739671 04
| Epoch (UTC): | 13 March 2026 01:01:06 |
| Eccentricity: | 0.5506252 |
| inclination: | 25.8134° |
| perigee height: | 286 km |
| apogee height: | 16617 km |
| right ascension of ascending node: | 349.9763° |
| argument of perigee: | 251.6872° |
| revolutions per day: | 4.80739671 |
| mean anomaly at epoch: | 43.2298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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