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 39133U 26088.16459432 +.00000000 +00000-0 +30016-3 0 00003
2 39133 64.8694 158.8206 0023077 248.3486 111.5187 15.25376171 04
| Epoch (UTC): | 29 March 2026 03:57:00 |
| Eccentricity: | 0.0023077 |
| inclination: | 64.8694° |
| perigee height: | 474 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 158.8206° |
| argument of perigee: | 248.3486° |
| revolutions per day: | 15.25376171 |
| mean anomaly at epoch: | 111.5187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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