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 28415U 04035C 24283.85309212 .00015728 00000-0 75187-3 0 9995
2 28415 97.4136 315.0968 0039827 347.1999 12.8220 15.18375370101349
| Epoch (UTC): | 09 October 2024 20:28:27 |
| Eccentricity: | 0.0039827 |
| inclination: | 97.4136° |
| perigee height: | 483 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 315.0968° |
| argument of perigee: | 347.1999° |
| revolutions per day: | 15.18375370 |
| mean anomaly at epoch: | 12.8220° |
| orbit number at epoch: | 10134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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