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 26339U 99057HY 24280.86435771 .00101857 00000-0 81678-2 0 9994
2 26339 98.1410 328.1696 0034689 207.4108 152.5284 14.99135539303120
| Epoch (UTC): | 06 October 2024 20:44:40 |
| Eccentricity: | 0.0034689 |
| inclination: | 98.1410° |
| perigee height: | 545 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 328.1696° |
| argument of perigee: | 207.4108° |
| revolutions per day: | 14.99135539 |
| mean anomaly at epoch: | 152.5284° |
| orbit number at epoch: | 30312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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