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 25194.34443452 .00000296 00000-0 99445-4 0 9994
2 00045 66.6922 176.2320 0244210 45.2406 316.8281 14.35574016331403
| Epoch (UTC): | 13 July 2025 08:15:59 |
| Eccentricity: | 0.0244210 |
| inclination: | 66.6922° |
| perigee height: | 598 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 176.2320° |
| argument of perigee: | 45.2406° |
| revolutions per day: | 14.35574016 |
| mean anomaly at epoch: | 316.8281° |
| orbit number at epoch: | 33140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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