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 70007U 26065.44701389 +.00000000 +00000-0 -21669-2 0 00009
2 70007 53.1602 78.8803 0000630 78.8877 102.2740 16.02090006 01
| Epoch (UTC): | 06 March 2026 10:43:42 |
| Eccentricity: | 0.0000630 |
| inclination: | 53.1602° |
| perigee height: | 268 km |
| apogee height: | 269 km |
| right ascension of ascending node: | 78.8803° |
| argument of perigee: | 78.8877° |
| revolutions per day: | 16.02090006 |
| mean anomaly at epoch: | 102.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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