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 27453U 26087.89860400 +.00000000 +00000-0 +12124-3 0 00005
2 27453 98.8574 52.7356 0010836 220.7073 139.3297 14.26200051 06
| Epoch (UTC): | 28 March 2026 21:33:59 |
| Eccentricity: | 0.0010836 |
| inclination: | 98.8574° |
| perigee height: | 797 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 52.7356° |
| argument of perigee: | 220.7073° |
| revolutions per day: | 14.26200051 |
| mean anomaly at epoch: | 139.3297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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