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 26022.49528883 +.00000000 +00000-0 +20316-3 0 00004
2 11870 74.0514 195.1564 0014977 85.5907 274.6958 14.38355115 00
| Epoch (UTC): | 22 January 2026 11:53:12 |
| Eccentricity: | 0.0014977 |
| inclination: | 74.0514° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 195.1564° |
| argument of perigee: | 85.5907° |
| revolutions per day: | 14.38355115 |
| mean anomaly at epoch: | 274.6958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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