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 59370U 26145.55509075 +.00000000 +00000-0 +23847-5 0 00000
2 59370 42.9996 174.9220 0001511 272.1035 87.9644 15.27583964 06
| Epoch (UTC): | 25 May 2026 13:19:19 |
| Eccentricity: | 0.0001511 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.9220° |
| argument of perigee: | 272.1035° |
| revolutions per day: | 15.27583964 |
| mean anomaly at epoch: | 87.9644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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