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 26074.51932697 +.00000000 +00000-0 +61853-4 0 00008
2 11870 74.0508 99.3870 0016610 332.6615 27.3663 14.38389572 06
| Epoch (UTC): | 15 March 2026 12:27:49 |
| Eccentricity: | 0.0016610 |
| inclination: | 74.0508° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 99.3870° |
| argument of perigee: | 332.6615° |
| revolutions per day: | 14.38389572 |
| mean anomaly at epoch: | 27.3663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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