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 62277U 26145.51507970 +.00000000 +00000-0 +21056-2 0 00005
2 62277 42.9999 313.6429 0001509 263.7516 96.3180 15.70939570 04
| Epoch (UTC): | 25 May 2026 12:21:42 |
| Eccentricity: | 0.0001509 |
| inclination: | 42.9999° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 313.6429° |
| argument of perigee: | 263.7516° |
| revolutions per day: | 15.70939570 |
| mean anomaly at epoch: | 96.3180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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