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 23332.39537199 .00005317 00000-0 59748-3 0 9996
2 00115 48.1653 330.5027 0032108 46.4641 313.8933 14.87616796378873
| Epoch (UTC): | 28 November 2023 09:29:20 |
| Eccentricity: | 0.0032108 |
| inclination: | 48.1653° |
| perigee height: | 583 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 330.5027° |
| argument of perigee: | 46.4641° |
| revolutions per day: | 14.87616796 |
| mean anomaly at epoch: | 313.8933° |
| orbit number at epoch: | 37887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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