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 55788U 26145.59746028 +.00000000 +00000-0 -13919-5 0 00004
2 55788 69.9996 10.6507 0002556 271.6021 88.4846 14.98329470 04
| Epoch (UTC): | 25 May 2026 14:20:20 |
| Eccentricity: | 0.0002556 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.6507° |
| argument of perigee: | 271.6021° |
| revolutions per day: | 14.98329470 |
| mean anomaly at epoch: | 88.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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