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 37766U 11039B 24357.70531995 .00001491 00000-0 25885-3 0 9999
2 37766 98.1610 246.3441 0042484 228.3302 131.4264 14.69141375717256
| Epoch (UTC): | 22 December 2024 16:55:39 |
| Eccentricity: | 0.0042484 |
| inclination: | 98.1610° |
| perigee height: | 634 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 246.3441° |
| argument of perigee: | 228.3302° |
| revolutions per day: | 14.69141375 |
| mean anomaly at epoch: | 131.4264° |
| orbit number at epoch: | 71725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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