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 33331U 26152.23491066 +.00000000 +00000-0 +11799-3 0 00003
2 33331 98.1237 226.3679 0005527 107.6452 252.5355 14.64708876 02
| Epoch (UTC): | 01 June 2026 05:38:16 |
| Eccentricity: | 0.0005527 |
| inclination: | 98.1237° |
| perigee height: | 674 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 226.3679° |
| argument of perigee: | 107.6452° |
| revolutions per day: | 14.64708876 |
| mean anomaly at epoch: | 252.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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