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 25682U 26071.99620206 +.00000000 +00000-0 +12785-3 0 00002
2 25682 97.8608 80.0383 0001665 80.5428 306.8172 14.63825950 00
| Epoch (UTC): | 12 March 2026 23:54:31 |
| Eccentricity: | 0.0001665 |
| inclination: | 97.8608° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 80.0383° |
| argument of perigee: | 80.5428° |
| revolutions per day: | 14.63825950 |
| mean anomaly at epoch: | 306.8172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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