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 23708U 26087.76998578 +.00000000 +00000-0 +56138-4 0 00002
2 23708 71.0511 200.2392 0184507 7.8591 155.5876 13.76713998 01
| Epoch (UTC): | 28 March 2026 18:28:46 |
| Eccentricity: | 0.0184507 |
| inclination: | 71.0511° |
| perigee height: | 840 km |
| apogee height: | 1111 km |
| right ascension of ascending node: | 200.2392° |
| argument of perigee: | 7.8591° |
| revolutions per day: | 13.76713998 |
| mean anomaly at epoch: | 155.5876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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