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 03338U 68066B 25073.47626212 .00000159 00000-0 15563-3 0 9998
2 03338 80.6565 78.4442 1130419 161.8390 202.6750 12.23393336522090
| Epoch (UTC): | 14 March 2025 11:25:49 |
| Eccentricity: | 0.1130419 |
| inclination: | 80.6565° |
| perigee height: | 678 km |
| apogee height: | 2477 km |
| right ascension of ascending node: | 78.4442° |
| argument of perigee: | 161.8390° |
| revolutions per day: | 12.23393336 |
| mean anomaly at epoch: | 202.6750° |
| orbit number at epoch: | 52209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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