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 10234U 26098.49188400 +.00000000 +00000-0 +51874-3 0 00000
2 10234 28.9458 243.2917 0276983 282.2445 74.7263 14.78293614 02
| Epoch (UTC): | 08 April 2026 11:48:18 |
| Eccentricity: | 0.0276983 |
| inclination: | 28.9458° |
| perigee height: | 440 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 243.2917° |
| argument of perigee: | 282.2445° |
| revolutions per day: | 14.78293614 |
| mean anomaly at epoch: | 74.7263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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