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 27939U 03042A 23158.73489017 .00001348 00000-0 24173-3 0 9993
2 27939 98.2422 305.6253 0012964 161.2749 322.2786 14.68370249 53153
| Epoch (UTC): | 07 June 2023 17:38:14 |
| Eccentricity: | 0.0012964 |
| inclination: | 98.2422° |
| perigee height: | 657 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 305.6253° |
| argument of perigee: | 161.2749° |
| revolutions per day: | 14.68370249 |
| mean anomaly at epoch: | 322.2786° |
| orbit number at epoch: | 5315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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