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 28054U 03048A 24358.13949649 .00000363 00000-0 21400-3 0 9993
2 28054 99.0199 6.4042 0006562 235.1994 211.9717 14.14234333 92980
| Epoch (UTC): | 23 December 2024 03:20:52 |
| Eccentricity: | 0.0006562 |
| inclination: | 99.0199° |
| perigee height: | 840 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 6.4042° |
| argument of perigee: | 235.1994° |
| revolutions per day: | 14.14234333 |
| mean anomaly at epoch: | 211.9717° |
| orbit number at epoch: | 9298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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