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 25338U 26071.99393359 +.00000000 +00000-0 +92338-4 0 00009
2 25338 98.5159 95.1889 0009052 269.1260 90.8884 14.27114082 09
| Epoch (UTC): | 12 March 2026 23:51:15 |
| Eccentricity: | 0.0009052 |
| inclination: | 98.5159° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 95.1889° |
| argument of perigee: | 269.1260° |
| revolutions per day: | 14.27114082 |
| mean anomaly at epoch: | 90.8884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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