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 26020.02403579 +.00000000 +00000-0 +59116-3 0 00006
2 28738 97.3618 33.5449 0004963 171.6669 188.4669 15.55774664 02
| Epoch (UTC): | 20 January 2026 00:34:36 |
| Eccentricity: | 0.0004963 |
| inclination: | 97.3618° |
| perigee height: | 397 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 33.5449° |
| argument of perigee: | 171.6669° |
| revolutions per day: | 15.55774664 |
| mean anomaly at epoch: | 188.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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