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 38122U 99025EPT 24257.82918660 .00011392 00000-0 26588-2 0 9998
2 38122 98.3216 266.0920 0240619 90.2678 272.6083 14.38632036611873
| Epoch (UTC): | 13 September 2024 19:54:01 |
| Eccentricity: | 0.0240619 |
| inclination: | 98.3216° |
| perigee height: | 591 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 266.0920° |
| argument of perigee: | 90.2678° |
| revolutions per day: | 14.38632036 |
| mean anomaly at epoch: | 272.6083° |
| orbit number at epoch: | 61187 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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