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 64777U 26145.55988558 +.00000000 +00000-0 +51460-3 0 00004
2 64777 53.1587 244.7927 0001078 93.0238 267.0888 15.34397977 02
| Epoch (UTC): | 25 May 2026 13:26:14 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.7927° |
| argument of perigee: | 93.0238° |
| revolutions per day: | 15.34397977 |
| mean anomaly at epoch: | 267.0888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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