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 42988U 26145.33737963 +.00000000 +00000-0 +27911-3 0 00006
2 42988 97.4473 281.9741 0001588 94.3223 265.8201 15.34183800 01
| Epoch (UTC): | 25 May 2026 08:05:49 |
| Eccentricity: | 0.0001588 |
| inclination: | 97.4473° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 281.9741° |
| argument of perigee: | 94.3223° |
| revolutions per day: | 15.34183800 |
| mean anomaly at epoch: | 265.8201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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