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 17295U 87003A 22147.78898056 .00004588 00000-0 22699-3 0 9995
2 17295 82.5120 165.9273 0003167 30.1330 330.0086 15.17579709932166
| Epoch (UTC): | 27 May 2022 18:56:07 |
| Eccentricity: | 0.0003167 |
| inclination: | 82.5120° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 165.9273° |
| argument of perigee: | 30.1330° |
| revolutions per day: | 15.17579709 |
| mean anomaly at epoch: | 330.0086° |
| orbit number at epoch: | 93216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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