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 33414U 26062.86819663 +.00000000 +00000-0 +00000-0 0 00001
2 33414 5.4888 74.2790 0065699 192.9010 189.5691 0.99274211 00
| Epoch (UTC): | 03 March 2026 20:50:12 |
| Eccentricity: | 0.0065699 |
| inclination: | 5.4888° |
| perigee height: | 35790 km |
| apogee height: | 36347 km |
| right ascension of ascending node: | 74.2790° |
| argument of perigee: | 192.9010° |
| revolutions per day: | 0.99274211 |
| mean anomaly at epoch: | 189.5691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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