▸Orbital parameters

Orbit class	SSO
Inclination	97.3754°
Eccentricity	0.0002979
Period	94.4 min
Apogee	493 km
Perigee	489 km
Mean motion	15.24990358 rev/day
RAAN	1.4370°
Arg of perigee	318.2891°
Mean anomaly	41.8120°
B*	3.7511e-4
Rev at epoch	49,101

▸Two-line element set (TLE)

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

1 42844U 17042V 26187.45718273 .00009291 00000-0 37511-3 0 9998

2 42844 97.3754 1.4370 0002979 318.2891 41.8120 15.24990358491010

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NANOACE",
  "OBJECT_ID": "2017-042V",
  "EPOCH": "2026-07-06T10:58:20.588+00:00",
  "MEAN_MOTION": 15.24990358,
  "ECCENTRICITY": 0.0002979,
  "INCLINATION": 97.3754,
  "RA_OF_ASC_NODE": 1.437,
  "ARG_OF_PERICENTER": 318.2891,
  "MEAN_ANOMALY": 41.812,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 42844,
  "REV_AT_EPOCH": 49101,
  "BSTAR": 0.00037511,
  "MEAN_MOTION_DOT": 0.00009291,
  "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	NANOACE
Operator	Tyvak Nanosatellite Systems LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jul 14, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.2HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/42844

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