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 26018.34201410 +.00000000 +00000-0 +15603-3 0 00006
2 29228 69.9335 7.2269 0005396 225.4849 134.5876 15.12389158 00
| Epoch (UTC): | 18 January 2026 08:12:30 |
| Eccentricity: | 0.0005396 |
| inclination: | 69.9335° |
| perigee height: | 525 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 7.2269° |
| argument of perigee: | 225.4849° |
| revolutions per day: | 15.12389158 |
| mean anomaly at epoch: | 134.5876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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