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 26069.34861992 +.00000000 +00000-0 +55233-4 0 00003
2 21938 82.9336 153.2725 0027686 296.8725 132.8821 13.75549547 04
| Epoch (UTC): | 10 March 2026 08:22:00 |
| Eccentricity: | 0.0027686 |
| inclination: | 82.9336° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 153.2725° |
| argument of perigee: | 296.8725° |
| revolutions per day: | 13.75549547 |
| mean anomaly at epoch: | 132.8821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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