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 49961U 26145.50307199 +.00000000 +00000-0 +11465-3 0 00004
2 49961 97.4058 115.1602 0000635 143.2348 216.8920 14.99379091 09
| Epoch (UTC): | 25 May 2026 12:04:25 |
| Eccentricity: | 0.0000635 |
| inclination: | 97.4058° |
| perigee height: | 568 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 115.1602° |
| argument of perigee: | 143.2348° |
| revolutions per day: | 14.99379091 |
| mean anomaly at epoch: | 216.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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