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 25399U 26053.24049226 +.00000000 +00000-0 +77144-4 0 00003
2 25399 98.9679 37.6282 0002870 85.4112 274.7394 14.25584901 09
| Epoch (UTC): | 22 February 2026 05:46:18 |
| Eccentricity: | 0.0002870 |
| inclination: | 98.9679° |
| perigee height: | 804 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 37.6282° |
| argument of perigee: | 85.4112° |
| revolutions per day: | 14.25584901 |
| mean anomaly at epoch: | 274.7394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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