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 19211U 26038.69946602 +.00000000 +00000-0 +75230-4 0 00009
2 19211 82.5273 126.5717 0021897 140.9711 219.3091 14.85352942 00
| Epoch (UTC): | 07 February 2026 16:47:13 |
| Eccentricity: | 0.0021897 |
| inclination: | 82.5273° |
| perigee height: | 597 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 126.5717° |
| argument of perigee: | 140.9711° |
| revolutions per day: | 14.85352942 |
| mean anomaly at epoch: | 219.3091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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