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 21398U 26072.57529773 +.00000000 +00000-0 +52813-4 0 00001
2 21398 82.5224 132.8494 0021472 149.8624 210.3830 14.81845509 01
| Epoch (UTC): | 13 March 2026 13:48:25 |
| Eccentricity: | 0.0021472 |
| inclination: | 82.5224° |
| perigee height: | 608 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 132.8494° |
| argument of perigee: | 149.8624° |
| revolutions per day: | 14.81845509 |
| mean anomaly at epoch: | 210.3830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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