▸Orbital parameters

Orbit class	SSO
Inclination	97.8890°
Eccentricity	0.0066249
Period	96.9 min
Apogee	655 km
Perigee	562 km
Mean motion	14.86713200 rev/day
RAAN	126.3363°
Arg of perigee	8.6556°
Mean anomaly	351.5786°
B*	3.1544e-4
Rev at epoch	67,903

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 39441U 13066AB 26187.25670691 .00002860 00000-0 31544-3 0 9993

2 39441 97.8890 126.3363 0066249 8.6556 351.5786 14.86713200679037

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NEE-02 KRYSAOR",
  "OBJECT_ID": "2013-066AB",
  "EPOCH": "2026-07-06T06:09:39.477+00:00",
  "MEAN_MOTION": 14.867132,
  "ECCENTRICITY": 0.00662493,
  "INCLINATION": 97.889,
  "RA_OF_ASC_NODE": 126.3363,
  "ARG_OF_PERICENTER": 8.6556,
  "MEAN_ANOMALY": 351.5786,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39441,
  "REV_AT_EPOCH": 67903,
  "BSTAR": 0.00031544349,
  "MEAN_MOTION_DOT": 0.0000286,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	NEE-02 KRYSAOR
Operator	Ecuadorian Civilian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog Ecuadorian Civilian Space AgencyMEDIUMvia Wikidata
Country	EcuadorMEDIUMvia Wikidata
Launch date	Nov 21, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/39441

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.