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 25479U 26088.02411145 +.00000000 +00000-0 +42297-3 0 00009
2 25479 45.0087 355.9679 0004040 251.5951 108.4459 14.38935580 00
| Epoch (UTC): | 29 March 2026 00:34:43 |
| Eccentricity: | 0.0004040 |
| inclination: | 45.0087° |
| perigee height: | 759 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 355.9679° |
| argument of perigee: | 251.5951° |
| revolutions per day: | 14.38935580 |
| mean anomaly at epoch: | 108.4459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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