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 00045U 60007A 25193.36908133 .00000281 00000-0 95928-4 0 9993
2 00045 66.6921 178.8099 0244150 45.9702 316.1229 14.35573207331262
| Epoch (UTC): | 12 July 2025 08:51:28 |
| Eccentricity: | 0.0244150 |
| inclination: | 66.6921° |
| perigee height: | 598 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 178.8099° |
| argument of perigee: | 45.9702° |
| revolutions per day: | 14.35573207 |
| mean anomaly at epoch: | 316.1229° |
| orbit number at epoch: | 33126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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