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 25107.95364921 .00000770 00000-0 21735-3 0 9991
2 00045 66.6949 44.5515 0242863 110.1478 252.5928 14.35481813319006
| Epoch (UTC): | 17 April 2025 22:53:15 |
| Eccentricity: | 0.0242863 |
| inclination: | 66.6949° |
| perigee height: | 600 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 44.5515° |
| argument of perigee: | 110.1478° |
| revolutions per day: | 14.35481813 |
| mean anomaly at epoch: | 252.5928° |
| orbit number at epoch: | 31900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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