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 42989U 26145.64537257 +.00000000 +00000-0 +29909-3 0 00004
2 42989 97.4392 283.0074 0008028 209.0792 151.0008 15.40923067 01
| Epoch (UTC): | 25 May 2026 15:29:20 |
| Eccentricity: | 0.0008028 |
| inclination: | 97.4392° |
| perigee height: | 438 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 283.0074° |
| argument of perigee: | 209.0792° |
| revolutions per day: | 15.40923067 |
| mean anomaly at epoch: | 151.0008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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