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 24258.80017511 .00006037 00000-0 10465-2 0 9992
2 28895 98.2133 34.8567 0016180 75.8719 284.4282 14.68546989 7834
| Epoch (UTC): | 14 September 2024 19:12:15 |
| Eccentricity: | 0.0016180 |
| inclination: | 98.2133° |
| perigee height: | 654 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 34.8567° |
| argument of perigee: | 75.8719° |
| revolutions per day: | 14.68546989 |
| mean anomaly at epoch: | 284.4282° |
| orbit number at epoch: | 783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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