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 25279U 26074.19513766 +.00000000 +00000-0 +17577-2 0 00004
2 25279 7.3441 74.4265 7009632 86.7640 344.4808 2.55798344 00
| Epoch (UTC): | 15 March 2026 04:40:59 |
| Eccentricity: | 0.7009632 |
| inclination: | 7.3441° |
| perigee height: | 375 km |
| apogee height: | 32037 km |
| right ascension of ascending node: | 74.4265° |
| argument of perigee: | 86.7640° |
| revolutions per day: | 2.55798344 |
| mean anomaly at epoch: | 344.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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