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 26065.86952668 +.00000000 +00000-0 +16113-3 0 00008
2 27453 98.8537 30.4694 0010633 290.7585 69.2454 14.26187432 06
| Epoch (UTC): | 06 March 2026 20:52:07 |
| Eccentricity: | 0.0010633 |
| inclination: | 98.8537° |
| perigee height: | 797 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 30.4694° |
| argument of perigee: | 290.7585° |
| revolutions per day: | 14.26187432 |
| mean anomaly at epoch: | 69.2454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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