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 26103.01383257 +.00000000 +00000-0 +30959-3 0 00002
2 23725 25.8067 320.1578 5507408 302.2889 15.8292 4.80952976 03
| Epoch (UTC): | 13 April 2026 00:19:55 |
| Eccentricity: | 0.5507408 |
| inclination: | 25.8067° |
| perigee height: | 282 km |
| apogee height: | 16612 km |
| right ascension of ascending node: | 320.1578° |
| argument of perigee: | 302.2889° |
| revolutions per day: | 4.80952976 |
| mean anomaly at epoch: | 15.8292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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