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 38494U 99025ESD 22180.59977208 .00002086 00000-0 10021-2 0 9995
2 38494 98.4390 240.8221 0479191 237.1107 118.3075 13.73072164495113
| Epoch (UTC): | 29 June 2022 14:23:40 |
| Eccentricity: | 0.0479191 |
| inclination: | 98.4390° |
| perigee height: | 635 km |
| apogee height: | 1341 km |
| right ascension of ascending node: | 240.8221° |
| argument of perigee: | 237.1107° |
| revolutions per day: | 13.73072164 |
| mean anomaly at epoch: | 118.3075° |
| orbit number at epoch: | 49511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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