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 28738U 26066.59265543 +.00000000 +00000-0 +68598-3 0 00009
2 28738 97.3596 81.6618 0006208 52.1217 308.0601 15.59917425 09
| Epoch (UTC): | 07 March 2026 14:13:25 |
| Eccentricity: | 0.0006208 |
| inclination: | 97.3596° |
| perigee height: | 384 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 81.6618° |
| argument of perigee: | 52.1217° |
| revolutions per day: | 15.59917425 |
| mean anomaly at epoch: | 308.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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