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 70020U 26065.41993056 +.00000000 +00000-0 -19043-2 0 00008
2 70020 53.1601 78.9944 0000544 73.3687 324.0431 16.03690966 08
| Epoch (UTC): | 06 March 2026 10:04:42 |
| Eccentricity: | 0.0000544 |
| inclination: | 53.1601° |
| perigee height: | 264 km |
| apogee height: | 265 km |
| right ascension of ascending node: | 78.9944° |
| argument of perigee: | 73.3687° |
| revolutions per day: | 16.03690966 |
| mean anomaly at epoch: | 324.0431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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