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 7228U 74013B 24358.10345054 .00001414 00000-0 39920-3 0 9994
2 7228 97.8409 226.3459 0104580 292.8078 66.2094 14.43976039660266
| Epoch (UTC): | 23 December 2024 02:28:58 |
| Eccentricity: | 0.0104580 |
| inclination: | 97.8409° |
| perigee height: | 671 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 226.3459° |
| argument of perigee: | 292.8078° |
| revolutions per day: | 14.43976039 |
| mean anomaly at epoch: | 66.2094° |
| orbit number at epoch: | 66026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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