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 24357.72889202 .00006649 00000-0 65152-3 0 9991
2 00115 48.1614 235.1278 0027545 344.5407 15.4665 14.92894597437077
| Epoch (UTC): | 22 December 2024 17:29:36 |
| Eccentricity: | 0.0027545 |
| inclination: | 48.1614° |
| perigee height: | 570 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 235.1278° |
| argument of perigee: | 344.5407° |
| revolutions per day: | 14.92894597 |
| mean anomaly at epoch: | 15.4665° |
| orbit number at epoch: | 43707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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