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 28485U 04047A 22146.57429478 .00004296 00000-0 25374-3 0 9998
2 28485 20.5564 103.9712 0010666 22.6225 337.4679 15.06311914960243
| Epoch (UTC): | 26 May 2022 13:46:59 |
| Eccentricity: | 0.0010666 |
| inclination: | 20.5564° |
| perigee height: | 540 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 103.9712° |
| argument of perigee: | 22.6225° |
| revolutions per day: | 15.06311914 |
| mean anomaly at epoch: | 337.4679° |
| orbit number at epoch: | 96024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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