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 25396U 26155.19541645 +.00000000 +00000-0 +89021-4 0 00006
2 25396 98.9858 145.9623 0002453 175.8840 184.2359 14.25757494 01
| Epoch (UTC): | 04 June 2026 04:41:23 |
| Eccentricity: | 0.0002453 |
| inclination: | 98.9858° |
| perigee height: | 804 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 145.9623° |
| argument of perigee: | 175.8840° |
| revolutions per day: | 14.25757494 |
| mean anomaly at epoch: | 184.2359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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