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 26017.16722895 +.00000000 +00000-0 +41871-4 0 00006
2 21423 82.4926 268.5059 0018311 53.4297 306.8599 14.81775693 05
| Epoch (UTC): | 17 January 2026 04:00:48 |
| Eccentricity: | 0.0018311 |
| inclination: | 82.4926° |
| perigee height: | 611 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 268.5059° |
| argument of perigee: | 53.4297° |
| revolutions per day: | 14.81775693 |
| mean anomaly at epoch: | 306.8599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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