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 26067.06099927 +.00000000 +00000-0 +28097-3 0 00005
2 36597 97.9911 93.2454 0047517 258.4509 101.1377 15.02321718 02
| Epoch (UTC): | 08 March 2026 01:27:50 |
| Eccentricity: | 0.0047517 |
| inclination: | 97.9911° |
| perigee height: | 527 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 93.2454° |
| argument of perigee: | 258.4509° |
| revolutions per day: | 15.02321718 |
| mean anomaly at epoch: | 101.1377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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