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 24262.86740017 .00003168 00000-0 52865-3 0 9995
2 27939 98.3026 60.6490 0012648 122.3582 343.7436 14.70630623122040
| Epoch (UTC): | 18 September 2024 20:49:03 |
| Eccentricity: | 0.0012648 |
| inclination: | 98.3026° |
| perigee height: | 650 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 60.6490° |
| argument of perigee: | 122.3582° |
| revolutions per day: | 14.70630623 |
| mean anomaly at epoch: | 343.7436° |
| orbit number at epoch: | 12204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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