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 21938U 26064.70290905 +.00000000 +00000-0 +96012-4 0 00008
2 21938 82.9341 156.7210 0027811 310.4040 166.8656 13.75548996 00
| Epoch (UTC): | 05 March 2026 16:52:11 |
| Eccentricity: | 0.0027811 |
| inclination: | 82.9341° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 156.7210° |
| argument of perigee: | 310.4040° |
| revolutions per day: | 13.75548996 |
| mean anomaly at epoch: | 166.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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