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 03597U 26053.81273543 +.00000000 +00000-0 +74331-4 0 00008
2 03597 34.9948 348.2840 0004860 77.7765 282.3470 14.47297733 02
| Epoch (UTC): | 22 February 2026 19:30:20 |
| Eccentricity: | 0.0004860 |
| inclination: | 34.9948° |
| perigee height: | 731 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 348.2840° |
| argument of perigee: | 77.7765° |
| revolutions per day: | 14.47297733 |
| mean anomaly at epoch: | 282.3470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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