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 26071.72169000 +.00000000 +00000-0 +51967-4 0 00004
2 26550 64.5627 213.7172 0506863 53.7253 310.9533 13.82063455 07
| Epoch (UTC): | 12 March 2026 17:19:14 |
| Eccentricity: | 0.0506863 |
| inclination: | 64.5627° |
| perigee height: | 585 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 213.7172° |
| argument of perigee: | 53.7253° |
| revolutions per day: | 13.82063455 |
| mean anomaly at epoch: | 310.9533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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