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 21873U 26144.89951064 +.00000000 +00000-0 +00000-0 0 00003
2 21873 14.8194 2.8784 0006218 336.2349 11.9642 0.99043103 08
| Epoch (UTC): | 24 May 2026 21:35:17 |
| Eccentricity: | 0.0006218 |
| inclination: | 14.8194° |
| perigee height: | 36108 km |
| apogee height: | 36161 km |
| right ascension of ascending node: | 2.8784° |
| argument of perigee: | 336.2349° |
| revolutions per day: | 0.99043103 |
| mean anomaly at epoch: | 11.9642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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