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 29U 60002B 22147.58542097 .00000289 00000-0 73609-4 0 9993
2 29 48.3783 201.5452 0023690 25.3065 334.9002 14.74637830323301
| Epoch (UTC): | 27 May 2022 14:03:00 |
| Eccentricity: | 0.0023690 |
| inclination: | 48.3783° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 201.5452° |
| argument of perigee: | 25.3065° |
| revolutions per day: | 14.74637830 |
| mean anomaly at epoch: | 334.9002° |
| orbit number at epoch: | 32330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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