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 33434U 26150.52700421 +.00000000 +00000-0 +18001-3 0 00008
2 33434 98.6143 176.9691 0013998 187.3490 172.7489 14.30150394 09
| Epoch (UTC): | 30 May 2026 12:38:53 |
| Eccentricity: | 0.0013998 |
| inclination: | 98.6143° |
| perigee height: | 781 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 176.9691° |
| argument of perigee: | 187.3490° |
| revolutions per day: | 14.30150394 |
| mean anomaly at epoch: | 172.7489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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