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 14690U 26076.21630007 +.00000000 +00000-0 +34580-3 0 00006
2 14690 63.2973 51.5552 0636519 123.3226 243.0453 14.13512077 06
| Epoch (UTC): | 17 March 2026 05:11:28 |
| Eccentricity: | 0.0636519 |
| inclination: | 63.2973° |
| perigee height: | 387 km |
| apogee height: | 1307 km |
| right ascension of ascending node: | 51.5552° |
| argument of perigee: | 123.3226° |
| revolutions per day: | 14.13512077 |
| mean anomaly at epoch: | 243.0453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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