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 55277U 26145.58725389 +.00000000 +00000-0 +10604-4 0 00009
2 55277 69.9990 210.5984 0003711 269.3750 90.6984 14.98330617 01
| Epoch (UTC): | 25 May 2026 14:05:38 |
| Eccentricity: | 0.0003711 |
| inclination: | 69.9990° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.5984° |
| argument of perigee: | 269.3750° |
| revolutions per day: | 14.98330617 |
| mean anomaly at epoch: | 90.6984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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