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 26075.14775089 +.00000000 +00000-0 +19738-3 0 00008
2 29228 69.9327 220.3162 0001202 152.5778 207.5452 15.12794613 01
| Epoch (UTC): | 16 March 2026 03:32:45 |
| Eccentricity: | 0.0001202 |
| inclination: | 69.9327° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 220.3162° |
| argument of perigee: | 152.5778° |
| revolutions per day: | 15.12794613 |
| mean anomaly at epoch: | 207.5452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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