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 25019U 26052.93682492 +.00000000 +00000-0 +00000-0 0 00008
2 25019 12.6467 22.5714 0006819 297.9029 56.5653 1.00271632 00
| Epoch (UTC): | 21 February 2026 22:29:01 |
| Eccentricity: | 0.0006819 |
| inclination: | 12.6467° |
| perigee height: | 35758 km |
| apogee height: | 35815 km |
| right ascension of ascending node: | 22.5714° |
| argument of perigee: | 297.9029° |
| revolutions per day: | 1.00271632 |
| mean anomaly at epoch: | 56.5653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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