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 61228U 24173B 24340.13618984 .00036766 00000-0 12251-2 0 9990
2 61228 97.3962 52.4077 0010933 28.9038 331.2807 15.30955422 10986
| Epoch (UTC): | 05 December 2024 03:16:06 |
| Eccentricity: | 0.0010933 |
| inclination: | 97.3962° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 52.4077° |
| argument of perigee: | 28.9038° |
| revolutions per day: | 15.30955422 |
| mean anomaly at epoch: | 331.2807° |
| orbit number at epoch: | 1098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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