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 14096U 26106.61848654 +.00000000 +00000-0 -52417-3 0 00003
2 14096 72.3026 329.5499 1091948 72.8206 298.9271 12.09983924 05
| Epoch (UTC): | 16 April 2026 14:50:37 |
| Eccentricity: | 0.1091948 |
| inclination: | 72.3026° |
| perigee height: | 761 km |
| apogee height: | 2512 km |
| right ascension of ascending node: | 329.5499° |
| argument of perigee: | 72.8206° |
| revolutions per day: | 12.09983924 |
| mean anomaly at epoch: | 298.9271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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