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 55282U 26145.28606770 +.00000000 +00000-0 +10423-1 0 00000
2 55282 69.9993 211.1496 0007730 239.8904 120.1490 14.99301867 00
| Epoch (UTC): | 25 May 2026 06:51:56 |
| Eccentricity: | 0.0007730 |
| inclination: | 69.9993° |
| perigee height: | 564 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 211.1496° |
| argument of perigee: | 239.8904° |
| revolutions per day: | 14.99301867 |
| mean anomaly at epoch: | 120.1490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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