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 28895U 05043F 24262.95635873 .00004080 00000-0 70962-3 0 9995
2 28895 98.2150 39.0307 0016046 63.4227 296.8620 14.68589304 8449
| Epoch (UTC): | 18 September 2024 22:57:09 |
| Eccentricity: | 0.0016046 |
| inclination: | 98.2150° |
| perigee height: | 654 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 39.0307° |
| argument of perigee: | 63.4227° |
| revolutions per day: | 14.68589304 |
| mean anomaly at epoch: | 296.8620° |
| orbit number at epoch: | 844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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