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 33495U 26150.80384420 +.00000000 +00000-0 +76935-4 0 00004
2 33495 98.1243 56.3796 0009053 86.1933 274.0310 14.74782335 07
| Epoch (UTC): | 30 May 2026 19:17:32 |
| Eccentricity: | 0.0009053 |
| inclination: | 98.1243° |
| perigee height: | 639 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 56.3796° |
| argument of perigee: | 86.1933° |
| revolutions per day: | 14.74782335 |
| mean anomaly at epoch: | 274.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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