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 19274U 26041.64020361 +.00000000 +00000-0 +33378-3 0 00008
2 19274 82.4703 290.4347 0011253 272.3364 87.6588 15.31107429 02
| Epoch (UTC): | 10 February 2026 15:21:53 |
| Eccentricity: | 0.0011253 |
| inclination: | 82.4703° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 290.4347° |
| argument of perigee: | 272.3364° |
| revolutions per day: | 15.31107429 |
| mean anomaly at epoch: | 87.6588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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