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 28737U 26150.06945979 +.00000000 +00000-0 +48080-3 0 00006
2 28737 97.7293 179.6892 0017581 95.8061 264.5179 15.21231306 07
| Epoch (UTC): | 30 May 2026 01:40:01 |
| Eccentricity: | 0.0017581 |
| inclination: | 97.7293° |
| perigee height: | 490 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 179.6892° |
| argument of perigee: | 95.8061° |
| revolutions per day: | 15.21231306 |
| mean anomaly at epoch: | 264.5179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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