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 00046U 60007B 25197.90352476 .00000499 00000-0 11269-3 0 9997
2 00046 66.6886 61.7387 0198049 187.4558 172.3600 14.54031648408246
| Epoch (UTC): | 16 July 2025 21:41:04 |
| Eccentricity: | 0.0198049 |
| inclination: | 66.6886° |
| perigee height: | 572 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 61.7387° |
| argument of perigee: | 187.4558° |
| revolutions per day: | 14.54031648 |
| mean anomaly at epoch: | 172.3600° |
| orbit number at epoch: | 40824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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