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 00309U 26088.20247115 +.00000000 +00000-0 +13586-3 0 00007
2 00309 58.0889 153.7419 0185983 154.2944 206.7475 14.60587715 00
| Epoch (UTC): | 29 March 2026 04:51:33 |
| Eccentricity: | 0.0185983 |
| inclination: | 58.0889° |
| perigee height: | 560 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 153.7419° |
| argument of perigee: | 154.2944° |
| revolutions per day: | 14.60587715 |
| mean anomaly at epoch: | 206.7475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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