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 26069U 00006A 22228.80033044 -.00000160 00000-0 -59690-4 0 9999
2 26069 70.9958 6.6054 0013448 253.9063 106.0579 14.13477078426048
| Epoch (UTC): | 16 August 2022 19:12:28 |
| Eccentricity: | 0.0013448 |
| inclination: | 70.9958° |
| perigee height: | 838 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 6.6054° |
| argument of perigee: | 253.9063° |
| revolutions per day: | 14.13477078 |
| mean anomaly at epoch: | 106.0579° |
| orbit number at epoch: | 42604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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