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 26155.06806993 +.00000000 +00000-0 +00000-0 0 00008
2 33414 5.7271 73.1665 0062948 193.9607 20.1962 0.99273455 05
| Epoch (UTC): | 04 June 2026 01:38:01 |
| Eccentricity: | 0.0062948 |
| inclination: | 5.7271° |
| perigee height: | 35802 km |
| apogee height: | 36336 km |
| right ascension of ascending node: | 73.1665° |
| argument of perigee: | 193.9607° |
| revolutions per day: | 0.99273455 |
| mean anomaly at epoch: | 20.1962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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