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 49445U 26145.23953523 +.00000000 +00000-0 +32262-4 0 00008
2 49445 53.2116 235.8668 0000900 91.8118 268.2977 15.08833538 06
| Epoch (UTC): | 25 May 2026 05:44:55 |
| Eccentricity: | 0.0000900 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 235.8668° |
| argument of perigee: | 91.8118° |
| revolutions per day: | 15.08833538 |
| mean anomaly at epoch: | 268.2977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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