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 42826U 26145.47000235 +.00000000 +00000-0 +36535-3 0 00009
2 42826 97.4432 313.7010 0007924 152.3761 207.7893 15.13753513 05
| Epoch (UTC): | 25 May 2026 11:16:48 |
| Eccentricity: | 0.0007924 |
| inclination: | 97.4432° |
| perigee height: | 519 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 313.7010° |
| argument of perigee: | 152.3761° |
| revolutions per day: | 15.13753513 |
| mean anomaly at epoch: | 207.7893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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