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 21423U 26159.44252733 +.00000000 +00000-0 +48082-4 0 00004
2 21423 82.4921 135.0961 0015711 306.3317 53.6446 14.81897004 03
| Epoch (UTC): | 08 June 2026 10:37:14 |
| Eccentricity: | 0.0015711 |
| inclination: | 82.4921° |
| perigee height: | 612 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 135.0961° |
| argument of perigee: | 306.3317° |
| revolutions per day: | 14.81897004 |
| mean anomaly at epoch: | 53.6446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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