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 29228U 26065.49374220 +.00000000 +00000-0 +21594-3 0 00000
2 29228 69.9310 245.2906 0002257 164.5852 195.5383 15.12716018 04
| Epoch (UTC): | 06 March 2026 11:50:59 |
| Eccentricity: | 0.0002257 |
| inclination: | 69.9310° |
| perigee height: | 526 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 245.2906° |
| argument of perigee: | 164.5852° |
| revolutions per day: | 15.12716018 |
| mean anomaly at epoch: | 195.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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