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 26715U 01009A 23080.94866079 .00000002 00000-0 00000+0 0 9994
2 26715 10.2792 26.0390 0001993 326.4590 43.9124 1.00269989 19787
| Epoch (UTC): | 21 March 2023 22:46:04 |
| Eccentricity: | 0.0001993 |
| inclination: | 10.2792° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 26.0390° |
| argument of perigee: | 326.4590° |
| revolutions per day: | 1.00269989 |
| mean anomaly at epoch: | 43.9124° |
| orbit number at epoch: | 1978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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