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 25030U 26155.32209080 +.00000000 +00000-0 +00000-0 0 00006
2 25030 55.5974 173.9656 0021666 261.4355 111.8353 1.88437838 03
| Epoch (UTC): | 04 June 2026 07:43:48 |
| Eccentricity: | 0.0021666 |
| inclination: | 55.5974° |
| perigee height: | 21250 km |
| apogee height: | 21370 km |
| right ascension of ascending node: | 173.9656° |
| argument of perigee: | 261.4355° |
| revolutions per day: | 1.88437838 |
| mean anomaly at epoch: | 111.8353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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