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 54079U 26145.61253523 +.00000000 +00000-0 +95057-4 0 00003
2 54079 53.2115 349.0228 0001339 89.5408 270.5738 15.08838179 04
| Epoch (UTC): | 25 May 2026 14:42:03 |
| Eccentricity: | 0.0001339 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 349.0228° |
| argument of perigee: | 89.5408° |
| revolutions per day: | 15.08838179 |
| mean anomaly at epoch: | 270.5738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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