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 42197U 26136.99307757 +.00000000 +00000-0 +69396-3 0 00007
2 42197 82.8480 41.8987 0116800 337.6871 21.9223 13.71298239 07
| Epoch (UTC): | 16 May 2026 23:50:01 |
| Eccentricity: | 0.0116800 |
| inclination: | 82.8480° |
| perigee height: | 909 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 41.8987° |
| argument of perigee: | 337.6871° |
| revolutions per day: | 13.71298239 |
| mean anomaly at epoch: | 21.9223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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