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 26905U 01040A 25172.88449966 0.00000300 00000-0 16934-3 0 00
2 26905 63.3680 96.7955 0620484 10.0095 349.9905 13.41459847 05
| Epoch (UTC): | 21 June 2025 21:13:40 |
| Eccentricity: | 0.0620484 |
| inclination: | 63.3680° |
| perigee height: | 639 km |
| apogee height: | 1568 km |
| right ascension of ascending node: | 96.7955° |
| argument of perigee: | 10.0095° |
| revolutions per day: | 13.41459847 |
| mean anomaly at epoch: | 349.9905° |
| 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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