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 25189.21057747 .00001947 00000-0 13436-3 0 9993
2 26474 67.9904 6.7031 0046812 311.1987 48.5129 15.07314682356121
| Epoch (UTC): | 08 July 2025 05:03:13 |
| Eccentricity: | 0.0046812 |
| inclination: | 67.9904° |
| perigee height: | 512 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 6.7031° |
| argument of perigee: | 311.1987° |
| revolutions per day: | 15.07314682 |
| mean anomaly at epoch: | 48.5129° |
| orbit number at epoch: | 35612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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