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 28372U 04025G 23084.20022847 .00000905 00000-0 24232-3 0 9995
2 28372 98.5362 52.9052 0046949 140.2109 220.2543 14.50058325990839
| Epoch (UTC): | 25 March 2023 04:48:19 |
| Eccentricity: | 0.0046949 |
| inclination: | 98.5362° |
| perigee height: | 692 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 52.9052° |
| argument of perigee: | 140.2109° |
| revolutions per day: | 14.50058325 |
| mean anomaly at epoch: | 220.2543° |
| orbit number at epoch: | 99083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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