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 25153.02803482 0.00000240 00000-0 12967-3 0 09
2 26907 63.3802 135.6939 0627927 10.2946 349.7808 13.42099279 04
| Epoch (UTC): | 02 June 2025 00:40:22 |
| Eccentricity: | 0.0627927 |
| inclination: | 63.3802° |
| perigee height: | 632 km |
| apogee height: | 1571 km |
| right ascension of ascending node: | 135.6939° |
| argument of perigee: | 10.2946° |
| revolutions per day: | 13.42099279 |
| mean anomaly at epoch: | 349.7808° |
| 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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