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 67300U 26145.14481061 +.00000000 +00000-0 +22484-3 0 00005
2 67300 97.4016 221.0361 0003815 45.7489 314.4062 15.25647358 00
| Epoch (UTC): | 25 May 2026 03:28:31 |
| Eccentricity: | 0.0003815 |
| inclination: | 97.4016° |
| perigee height: | 486 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 221.0361° |
| argument of perigee: | 45.7489° |
| revolutions per day: | 15.25647358 |
| mean anomaly at epoch: | 314.4062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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