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 00051U 60009C 25140.40237918 -.00000073 00000-0 12145-3 0 9994
2 00051 47.2098 184.7627 0106421 109.7232 251.5071 12.18359158883284
| Epoch (UTC): | 20 May 2025 09:39:25 |
| Eccentricity: | 0.0106421 |
| inclination: | 47.2098° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 184.7627° |
| argument of perigee: | 109.7232° |
| revolutions per day: | 12.18359158 |
| mean anomaly at epoch: | 251.5071° |
| orbit number at epoch: | 88328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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