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 26140.38720529 +.00000000 +00000-0 +00000-0 0 00003
2 21873 14.8182 2.9113 0006187 332.7691 206.4947 0.99042923 06
| Epoch (UTC): | 20 May 2026 09:17:34 |
| Eccentricity: | 0.0006187 |
| inclination: | 14.8182° |
| perigee height: | 36108 km |
| apogee height: | 36161 km |
| right ascension of ascending node: | 2.9113° |
| argument of perigee: | 332.7691° |
| revolutions per day: | 0.99042923 |
| mean anomaly at epoch: | 206.4947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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