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 data is extracted from the following two-line orbital elements,
1 31126U 07012K 23341.58413084 .00001282 00000-0 27094-3 0 9997
2 31126 98.3107 283.4536 0088279 37.4868 323.2443 14.58689063884173
| Epoch (UTC): | 07 December 2023 14:01:08 |
| Eccentricity: | 0.0088279 |
| inclination: | 98.3107° |
| perigee height: | 635 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 283.4536° |
| argument of perigee: | 37.4868° |
| revolutions per day: | 14.58689063 |
| mean anomaly at epoch: | 323.2443° |
| orbit number at epoch: | 88417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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