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 23613U 26145.03106889 +.00000000 +00000-0 +00000-0 0 00001
2 23613 13.3871 348.3510 0011130 72.6341 282.0830 1.00270588 07
| Epoch (UTC): | 25 May 2026 00:44:44 |
| Eccentricity: | 0.0011130 |
| inclination: | 13.3871° |
| perigee height: | 35740 km |
| apogee height: | 35834 km |
| right ascension of ascending node: | 348.3510° |
| argument of perigee: | 72.6341° |
| revolutions per day: | 1.00270588 |
| mean anomaly at epoch: | 282.0830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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