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 26067.59383877 +.00000000 +00000-0 +26941-3 0 00009
2 36597 97.9913 93.7947 0047507 256.5723 103.0204 15.02325227 01
| Epoch (UTC): | 08 March 2026 14:15:07 |
| Eccentricity: | 0.0047507 |
| inclination: | 97.9913° |
| perigee height: | 527 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 93.7947° |
| argument of perigee: | 256.5723° |
| revolutions per day: | 15.02325227 |
| mean anomaly at epoch: | 103.0204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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