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 55636U 26145.62248437 +.00000000 +00000-0 +20726-4 0 00003
2 55636 70.0003 10.4151 0002702 269.1802 90.9048 14.98329083 05
| Epoch (UTC): | 25 May 2026 14:56:22 |
| Eccentricity: | 0.0002702 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.4151° |
| argument of perigee: | 269.1802° |
| revolutions per day: | 14.98329083 |
| mean anomaly at epoch: | 90.9048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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