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 is defined by the following mean orbital elements,
1 14241U 26106.38572897 +.00000000 +00000-0 +18138-4 0 00004
2 14241 74.0570 88.2211 0015481 75.6495 284.6376 14.37541149 09
| Epoch (UTC): | 16 April 2026 09:15:26 |
| Eccentricity: | 0.0015481 |
| inclination: | 74.0570° |
| perigee height: | 756 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 88.2211° |
| argument of perigee: | 75.6495° |
| revolutions per day: | 14.37541149 |
| mean anomaly at epoch: | 284.6376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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