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 25114U 97084C 23337.68435110 .00002409 00000-0 77883-3 0 9998
2 25114 45.0121 175.5968 0005289 263.4170 96.6078 14.41474333360386
| Epoch (UTC): | 03 December 2023 16:25:27 |
| Eccentricity: | 0.0005289 |
| inclination: | 45.0121° |
| perigee height: | 750 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 175.5968° |
| argument of perigee: | 263.4170° |
| revolutions per day: | 14.41474333 |
| mean anomaly at epoch: | 96.6078° |
| orbit number at epoch: | 36038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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