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 17997U 87043A 23259.80622979 0.00023000 00000-0 11218-2 0 02
2 17997 63.2780 154.0856 0890116 86.8303 272.7975 13.68942262 05
| Epoch (UTC): | 16 September 2023 19:20:58 |
| Eccentricity: | 0.0890116 |
| inclination: | 63.2780° |
| perigee height: | 346 km |
| apogee height: | 1660 km |
| right ascension of ascending node: | 154.0856° |
| argument of perigee: | 86.8303° |
| revolutions per day: | 13.68942262 |
| mean anomaly at epoch: | 272.7975° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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