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 29047U 26053.69645322 +.00000000 +00000-0 +21021-3 0 00007
2 29047 71.9770 186.0475 0046716 75.7542 284.8778 14.31293135 06
| Epoch (UTC): | 22 February 2026 16:42:53 |
| Eccentricity: | 0.0046716 |
| inclination: | 71.9770° |
| perigee height: | 754 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 186.0475° |
| argument of perigee: | 75.7542° |
| revolutions per day: | 14.31293135 |
| mean anomaly at epoch: | 284.8778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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