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 00016U 58002A 23030.05330598 .00000043 00000-0 46368-4 0 9991
2 00016 34.2728 272.2518 2027236 311.4720 32.8366 10.48809260559276
| Epoch (UTC): | 30 January 2023 01:16:45 |
| Eccentricity: | 0.2027236 |
| inclination: | 34.2728° |
| perigee height: | 650 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 272.2518° |
| argument of perigee: | 311.4720° |
| revolutions per day: | 10.48809260 |
| mean anomaly at epoch: | 32.8366° |
| orbit number at epoch: | 55927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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