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 40069U 26044.96129215 +.00000000 +00000-0 -50721-4 0 00003
2 40069 98.4983 25.1515 0006612 42.4646 317.7042 14.21417787 08
| Epoch (UTC): | 13 February 2026 23:04:15 |
| Eccentricity: | 0.0006612 |
| inclination: | 98.4983° |
| perigee height: | 816 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 25.1515° |
| argument of perigee: | 42.4646° |
| revolutions per day: | 14.21417787 |
| mean anomaly at epoch: | 317.7042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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