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 26474U 00047B 25197.90321127 .00001939 00000-0 13369-3 0 9990
2 26474 67.9913 342.3440 0047355 302.3165 57.3401 15.07350332357356
| Epoch (UTC): | 16 July 2025 21:40:37 |
| Eccentricity: | 0.0047355 |
| inclination: | 67.9913° |
| perigee height: | 511 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 342.3440° |
| argument of perigee: | 302.3165° |
| revolutions per day: | 15.07350332 |
| mean anomaly at epoch: | 57.3401° |
| orbit number at epoch: | 35735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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