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 26145.52934963 +.00000000 +00000-0 +12408-3 0 00009
2 28649 97.5320 169.6216 0002532 108.7207 251.4287 14.90979652 06
| Epoch (UTC): | 25 May 2026 12:42:15 |
| Eccentricity: | 0.0002532 |
| inclination: | 97.5320° |
| perigee height: | 593 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 169.6216° |
| argument of perigee: | 108.7207° |
| revolutions per day: | 14.90979652 |
| mean anomaly at epoch: | 251.4287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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