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 56723U 26145.58362434 +.00000000 +00000-0 -35393-4 0 00007
2 56723 87.8989 263.7261 0001590 90.0389 270.0924 13.15547247 08
| Epoch (UTC): | 25 May 2026 14:00:25 |
| Eccentricity: | 0.0001590 |
| inclination: | 87.8989° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7261° |
| argument of perigee: | 90.0389° |
| revolutions per day: | 13.15547247 |
| mean anomaly at epoch: | 270.0924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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