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 18152U 87055A 22228.44877117 .00001334 00000-0 84794-4 0 9994
2 18152 82.4954 257.7352 0013331 236.2563 123.7396 15.07972273892485
| Epoch (UTC): | 16 August 2022 10:46:13 |
| Eccentricity: | 0.0013331 |
| inclination: | 82.4954° |
| perigee height: | 533 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 257.7352° |
| argument of perigee: | 236.2563° |
| revolutions per day: | 15.07972273 |
| mean anomaly at epoch: | 123.7396° |
| orbit number at epoch: | 89248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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