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 00115U 60002D 23036.77665447 .00002576 00000-0 31970-3 0 9998
2 00115 48.1663 318.5448 0033629 178.2597 181.8439 14.85291212334898
| Epoch (UTC): | 05 February 2023 18:38:22 |
| Eccentricity: | 0.0033629 |
| inclination: | 48.1663° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 318.5448° |
| argument of perigee: | 178.2597° |
| revolutions per day: | 14.85291212 |
| mean anomaly at epoch: | 181.8439° |
| orbit number at epoch: | 33489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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