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 24261.18488497 .00011506 00000-0 19834-2 0 9998
2 28895 98.2143 37.2514 0016083 68.5872 291.7047 14.68584953 8187
| Epoch (UTC): | 17 September 2024 04:26:14 |
| Eccentricity: | 0.0016083 |
| inclination: | 98.2143° |
| perigee height: | 654 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 37.2514° |
| argument of perigee: | 68.5872° |
| revolutions per day: | 14.68584953 |
| mean anomaly at epoch: | 291.7047° |
| orbit number at epoch: | 818 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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