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 26033U 26150.40111164 +.00000000 +00000-0 +13639-3 0 00004
2 26033 98.3428 295.1186 0026763 160.4336 199.7900 14.65902207 00
| Epoch (UTC): | 30 May 2026 09:37:36 |
| Eccentricity: | 0.0026763 |
| inclination: | 98.3428° |
| perigee height: | 655 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 295.1186° |
| argument of perigee: | 160.4336° |
| revolutions per day: | 14.65902207 |
| mean anomaly at epoch: | 199.7900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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