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 42839U 26145.43224627 +.00000000 +00000-0 +54810-3 0 00008
2 42839 97.4078 326.1827 0008022 80.4074 279.8072 15.27278859 06
| Epoch (UTC): | 25 May 2026 10:22:26 |
| Eccentricity: | 0.0008022 |
| inclination: | 97.4078° |
| perigee height: | 478 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 326.1827° |
| argument of perigee: | 80.4074° |
| revolutions per day: | 15.27278859 |
| mean anomaly at epoch: | 279.8072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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