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 33410U 08053C 22147.57502059 .00002682 00000-0 18451-3 0 9996
2 33410 97.8988 153.8846 0125357 261.2150 97.4860 15.00647780741045
| Epoch (UTC): | 27 May 2022 13:48:01 |
| Eccentricity: | 0.0125357 |
| inclination: | 97.8988° |
| perigee height: | 478 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 153.8846° |
| argument of perigee: | 261.2150° |
| revolutions per day: | 15.00647780 |
| mean anomaly at epoch: | 97.4860° |
| orbit number at epoch: | 74104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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