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 26161.47829478 +.00000000 +00000-0 +25533-3 0 00002
2 19210 82.5081 64.7985 0011612 146.9361 213.2608 15.29882560 07
| Epoch (UTC): | 10 June 2026 11:28:44 |
| Eccentricity: | 0.0011612 |
| inclination: | 82.5081° |
| perigee height: | 468 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.7985° |
| argument of perigee: | 146.9361° |
| revolutions per day: | 15.29882560 |
| mean anomaly at epoch: | 213.2608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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