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 23342.20122225 .00002309 00000-0 27334-3 0 9991
2 00115 48.1648 283.0466 0031886 90.8246 269.6322 14.87719800380336
Epoch (UTC): | 08 December 2023 04:49:45 |
Eccentricity: | 0.0031886 |
inclination: | 48.1648° |
perigee height: | 583 km |
apogee height: | 627 km |
right ascension of ascending node: | 283.0466° |
argument of perigee: | 90.8246° |
revolutions per day: | 14.87719800 |
mean anomaly at epoch: | 269.6322° |
orbit number at epoch: | 38033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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