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 49310U 26145.33202721 +.00000000 +00000-0 +18419-3 0 00004
2 49310 87.9178 279.0350 0002315 91.7465 268.3933 13.20811387 06
| Epoch (UTC): | 25 May 2026 07:58:07 |
| Eccentricity: | 0.0002315 |
| inclination: | 87.9178° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0350° |
| argument of perigee: | 91.7465° |
| revolutions per day: | 13.20811387 |
| mean anomaly at epoch: | 268.3933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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