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 03307U 26031.24689312 +.00000000 +00000-0 +00000-0 0 00003
2 03307 120.8433 91.3182 0016039 281.5202 78.3599 6.42444850 07
| Epoch (UTC): | 31 January 2026 05:55:31 |
| Eccentricity: | 0.0016039 |
| inclination: | 120.8433° |
| perigee height: | 5825 km |
| apogee height: | 5864 km |
| right ascension of ascending node: | 91.3182° |
| argument of perigee: | 281.5202° |
| revolutions per day: | 6.42444850 |
| mean anomaly at epoch: | 78.3599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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