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 25416U 26145.29587302 +.00000000 +00000-0 +25735-3 0 00000
2 25416 44.9954 0.0384 0000359 155.0677 205.0189 14.38027660 00
| Epoch (UTC): | 25 May 2026 07:06:03 |
| Eccentricity: | 0.0000359 |
| inclination: | 44.9954° |
| perigee height: | 765 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 0.0384° |
| argument of perigee: | 155.0677° |
| revolutions per day: | 14.38027660 |
| mean anomaly at epoch: | 205.0189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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