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 07005U 26087.99905744 +.00000000 +00000-0 +51391-4 0 00008
2 07005 65.4375 298.5729 0040696 92.7672 267.8052 13.85512871 05
| Epoch (UTC): | 28 March 2026 23:58:38 |
| Eccentricity: | 0.0040696 |
| inclination: | 65.4375° |
| perigee height: | 915 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 298.5729° |
| argument of perigee: | 92.7672° |
| revolutions per day: | 13.85512871 |
| mean anomaly at epoch: | 267.8052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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