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 26073.60302064 +.00000000 +00000-0 +40975-4 0 00009
2 26550 64.5629 208.7569 0506966 53.2535 311.3970 13.82063944 08
| Epoch (UTC): | 14 March 2026 14:28:20 |
| Eccentricity: | 0.0506966 |
| inclination: | 64.5629° |
| perigee height: | 585 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 208.7569° |
| argument of perigee: | 53.2535° |
| revolutions per day: | 13.82063944 |
| mean anomaly at epoch: | 311.3970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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