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 26486U 00051D 23144.47970885 -.00000208 00000-0 00000-0 0 9995
2 26486 63.1115 316.5067 7436752 276.0710 10.9706 1.45765046120914
| Epoch (UTC): | 24 May 2023 11:30:46 |
| Eccentricity: | 0.7436752 |
| inclination: | 63.1115° |
| perigee height: | 2044 km |
| apogee height: | 50914 km |
| right ascension of ascending node: | 316.5067° |
| argument of perigee: | 276.0710° |
| revolutions per day: | 1.45765046 |
| mean anomaly at epoch: | 10.9706° |
| orbit number at epoch: | 12091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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