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 26550U 26064.55815284 +.00000000 +00000-0 +36503-4 0 00008
2 26550 64.5614 232.6050 0506367 55.5330 309.2494 13.82060812 04
| Epoch (UTC): | 05 March 2026 13:23:44 |
| Eccentricity: | 0.0506367 |
| inclination: | 64.5614° |
| perigee height: | 585 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 232.6050° |
| argument of perigee: | 55.5330° |
| revolutions per day: | 13.82060812 |
| mean anomaly at epoch: | 309.2494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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