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 54799U 26145.41516433 +.00000000 +00000-0 +22263-4 0 00001
2 54799 53.2151 34.6465 0001034 91.3118 268.7993 15.08838219 01
| Epoch (UTC): | 25 May 2026 09:57:50 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 34.6465° |
| argument of perigee: | 91.3118° |
| revolutions per day: | 15.08838219 |
| mean anomaly at epoch: | 268.7993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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