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 36597U 26072.98878105 +.00000000 +00000-0 +18474-3 0 00003
2 36597 97.9904 99.3544 0047669 237.7629 121.8970 15.02354791 07
| Epoch (UTC): | 13 March 2026 23:43:50 |
| Eccentricity: | 0.0047669 |
| inclination: | 97.9904° |
| perigee height: | 527 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 99.3544° |
| argument of perigee: | 237.7629° |
| revolutions per day: | 15.02354791 |
| mean anomaly at epoch: | 121.8970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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