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 15360U 84109B 23033.31875809 .00000065 00000-0 50044-4 0 9997
2 15360 82.9424 320.6885 0042623 62.6017 297.9466 13.76824519924247
| Epoch (UTC): | 02 February 2023 07:39:00 |
| Eccentricity: | 0.0042623 |
| inclination: | 82.9424° |
| perigee height: | 944 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 320.6885° |
| argument of perigee: | 62.6017° |
| revolutions per day: | 13.76824519 |
| mean anomaly at epoch: | 297.9466° |
| orbit number at epoch: | 92424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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