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 19210U 26073.60079219 +.00000000 +00000-0 +34927-3 0 00006
2 19210 82.5102 153.3084 0012589 107.0522 253.2098 15.28617844 04
| Epoch (UTC): | 14 March 2026 14:25:08 |
| Eccentricity: | 0.0012589 |
| inclination: | 82.5102° |
| perigee height: | 471 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 153.3084° |
| argument of perigee: | 107.0522° |
| revolutions per day: | 15.28617844 |
| mean anomaly at epoch: | 253.2098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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