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 26907U 01040C 21106.97234151 0.00000024 00000-0 20697-4 0 08
2 26907 63.4042 46.6589 0497554 2.2793 357.7207 13.41331086 01
| Epoch (UTC): | 16 April 2021 23:20:10 |
| Eccentricity: | 0.0497554 |
| inclination: | 63.4042° |
| perigee height: | 732 km |
| apogee height: | 1476 km |
| right ascension of ascending node: | 46.6589° |
| argument of perigee: | 2.2793° |
| revolutions per day: | 13.41331086 |
| mean anomaly at epoch: | 357.7207° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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