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 33278U 26145.13649310 +.00000000 +00000-0 +00000-0 0 00001
2 33278 4.2739 31.5396 0002850 32.2105 130.1141 1.00269890 01
| Epoch (UTC): | 25 May 2026 03:16:33 |
| Eccentricity: | 0.0002850 |
| inclination: | 4.2739° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 31.5396° |
| argument of perigee: | 32.2105° |
| revolutions per day: | 1.00269890 |
| mean anomaly at epoch: | 130.1141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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