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 62461U 24253C 25093.60098506 .06123810 12042-4 53849-3 0 9994
2 62461 55.1994 162.5248 0005929 311.9454 141.1615 16.38452900 14905
| Epoch (UTC): | 03 April 2025 14:25:25 |
| Eccentricity: | 0.0005929 |
| inclination: | 55.1994° |
| perigee height: | 166 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 162.5248° |
| argument of perigee: | 311.9454° |
| revolutions per day: | 16.38452900 |
| mean anomaly at epoch: | 141.1615° |
| orbit number at epoch: | 1490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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