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 25107.78265036 .00005282 00000-0 50050-3 0 9997
2 00115 48.1641 28.0906 0027517 145.3466 214.9251 14.94612616454422
| Epoch (UTC): | 17 April 2025 18:47:00 |
| Eccentricity: | 0.0027517 |
| inclination: | 48.1641° |
| perigee height: | 564 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 28.0906° |
| argument of perigee: | 145.3466° |
| revolutions per day: | 14.94612616 |
| mean anomaly at epoch: | 214.9251° |
| orbit number at epoch: | 45442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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