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 26073.00611464 +.00000000 +00000-0 +59547-3 0 00004
2 28738 97.3594 88.3119 0005160 35.6618 324.4983 15.60561597 06
| Epoch (UTC): | 14 March 2026 00:08:48 |
| Eccentricity: | 0.0005160 |
| inclination: | 97.3594° |
| perigee height: | 383 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 88.3119° |
| argument of perigee: | 35.6618° |
| revolutions per day: | 15.60561597 |
| mean anomaly at epoch: | 324.4983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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