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 24257.36932706 .00010280 00000-0 17754-2 0 9997
2 28895 98.2129 33.4202 0016172 80.0753 280.2276 14.68530529 7624
| Epoch (UTC): | 13 September 2024 08:51:49 |
| Eccentricity: | 0.0016172 |
| inclination: | 98.2129° |
| perigee height: | 654 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 33.4202° |
| argument of perigee: | 80.0753° |
| revolutions per day: | 14.68530529 |
| mean anomaly at epoch: | 280.2276° |
| orbit number at epoch: | 762 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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