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 62197U 26145.42932854 +.00000000 +00000-0 +65393-3 0 00002
2 62197 42.9995 197.6756 0000641 304.6186 55.4605 15.27604595 04
| Epoch (UTC): | 25 May 2026 10:18:13 |
| Eccentricity: | 0.0000641 |
| inclination: | 42.9995° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 197.6756° |
| argument of perigee: | 304.6186° |
| revolutions per day: | 15.27604595 |
| mean anomaly at epoch: | 55.4605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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