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 24281.81009766 .00020489 00000-0 97968-3 0 9991
2 28415 97.4136 313.0945 0040099 354.5250 5.5540 15.18301213101032
| Epoch (UTC): | 07 October 2024 19:26:32 |
| Eccentricity: | 0.0040099 |
| inclination: | 97.4136° |
| perigee height: | 483 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 313.0945° |
| argument of perigee: | 354.5250° |
| revolutions per day: | 15.18301213 |
| mean anomaly at epoch: | 5.5540° |
| orbit number at epoch: | 10103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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