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 08520U 26074.14161563 +.00000000 +00000-0 +13559-3 0 00000
2 08520 81.2895 320.6284 0027617 319.2784 40.6321 14.09425855 01
| Epoch (UTC): | 15 March 2026 03:23:55 |
| Eccentricity: | 0.0027617 |
| inclination: | 81.2895° |
| perigee height: | 841 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 320.6284° |
| argument of perigee: | 319.2784° |
| revolutions per day: | 14.09425855 |
| mean anomaly at epoch: | 40.6321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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