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 28894U 05043E 24259.92328775 .00002938 00000-0 57191-3 0 9996
2 28894 98.2215 26.2684 0017315 122.4236 237.8644 14.63733412 6694
| Epoch (UTC): | 15 September 2024 22:09:32 |
| Eccentricity: | 0.0017315 |
| inclination: | 98.2215° |
| perigee height: | 669 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 26.2684° |
| argument of perigee: | 122.4236° |
| revolutions per day: | 14.63733412 |
| mean anomaly at epoch: | 237.8644° |
| orbit number at epoch: | 669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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