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 54791U 26145.41793291 +.00000000 +00000-0 +38663-3 0 00002
2 54791 53.2127 44.6172 0001211 95.3573 264.7557 15.08803238 03
| Epoch (UTC): | 25 May 2026 10:01:49 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.6172° |
| argument of perigee: | 95.3573° |
| revolutions per day: | 15.08803238 |
| mean anomaly at epoch: | 264.7557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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