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 51977U 26145.39037448 +.00000000 +00000-0 +35281-3 0 00000
2 51977 53.2129 34.8048 0001591 91.5930 268.5245 15.08812393 05
| Epoch (UTC): | 25 May 2026 09:22:08 |
| Eccentricity: | 0.0001591 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.8048° |
| argument of perigee: | 91.5930° |
| revolutions per day: | 15.08812393 |
| mean anomaly at epoch: | 268.5245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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