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 21231U 26044.73417266 +.00000000 +00000-0 +66068-4 0 00004
2 21231 82.9507 284.7896 0036055 31.6618 32.0428 13.76110224 06
| Epoch (UTC): | 13 February 2026 17:37:12 |
| Eccentricity: | 0.0036055 |
| inclination: | 82.9507° |
| perigee height: | 951 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 284.7896° |
| argument of perigee: | 31.6618° |
| revolutions per day: | 13.76110224 |
| mean anomaly at epoch: | 32.0428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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