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 10820U 26069.11557382 +.00000000 +00000-0 +20686-3 0 00004
2 10820 98.4534 265.5651 0008233 285.7444 74.2835 14.37989165 08
| Epoch (UTC): | 10 March 2026 02:46:25 |
| Eccentricity: | 0.0008233 |
| inclination: | 98.4534° |
| perigee height: | 759 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 265.5651° |
| argument of perigee: | 285.7444° |
| revolutions per day: | 14.37989165 |
| mean anomaly at epoch: | 74.2835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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