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 29273U 26150.54160817 +.00000000 +00000-0 +00000-0 0 00002
2 29273 2.8621 80.4013 0003779 311.7680 288.8875 0.98626091 09
| Epoch (UTC): | 30 May 2026 12:59:54 |
| Eccentricity: | 0.0003779 |
| inclination: | 2.8621° |
| perigee height: | 36238 km |
| apogee height: | 36270 km |
| right ascension of ascending node: | 80.4013° |
| argument of perigee: | 311.7680° |
| revolutions per day: | 0.98626091 |
| mean anomaly at epoch: | 288.8875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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