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 11870U 26073.54562450 +.00000000 +00000-0 +70836-4 0 00007
2 11870 74.0509 101.1798 0016580 334.5953 25.4385 14.38389319 09
| Epoch (UTC): | 14 March 2026 13:05:41 |
| Eccentricity: | 0.0016580 |
| inclination: | 74.0509° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 101.1798° |
| argument of perigee: | 334.5953° |
| revolutions per day: | 14.38389319 |
| mean anomaly at epoch: | 25.4385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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