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 26102U 00014A 22134.07156250 .13335860 26964-5 14383-3 0 9997
2 26102 97.4395 68.1275 0009975 232.3535 322.2781 16.50257195233253
| Epoch (UTC): | 14 May 2022 01:43:03 |
| Eccentricity: | 0.0009975 |
| inclination: | 97.4395° |
| perigee height: | 132 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 68.1275° |
| argument of perigee: | 232.3535° |
| revolutions per day: | 16.50257195 |
| mean anomaly at epoch: | 322.2781° |
| orbit number at epoch: | 23325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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