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 28649U 26074.65537495 +.00000000 +00000-0 +14002-3 0 00005
2 28649 97.5409 101.9365 0002120 62.2962 297.8472 14.90786928 05
| Epoch (UTC): | 15 March 2026 15:43:44 |
| Eccentricity: | 0.0002120 |
| inclination: | 97.5409° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 101.9365° |
| argument of perigee: | 62.2962° |
| revolutions per day: | 14.90786928 |
| mean anomaly at epoch: | 297.8472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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