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 40362U 26145.62162814 +.00000000 +00000-0 +32467-3 0 00001
2 40362 97.0646 146.3758 0006586 117.3724 242.8198 15.46319618 01
| Epoch (UTC): | 25 May 2026 14:55:08 |
| Eccentricity: | 0.0006586 |
| inclination: | 97.0646° |
| perigee height: | 423 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 146.3758° |
| argument of perigee: | 117.3724° |
| revolutions per day: | 15.46319618 |
| mean anomaly at epoch: | 242.8198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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