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 49728U 26145.47220628 +.00000000 +00000-0 +11851-4 0 00002
2 49728 53.2110 174.4286 0000778 92.6781 267.4300 15.08841819 08
| Epoch (UTC): | 25 May 2026 11:19:58 |
| Eccentricity: | 0.0000778 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.4286° |
| argument of perigee: | 92.6781° |
| revolutions per day: | 15.08841819 |
| mean anomaly at epoch: | 267.4300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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